JOHN F. BUTTS 8c ASSOC., INC. CONSULTING ENGINEERS 2480 VANTAGE DRIVE COLORADO SPRINGS, CO (719) FAX (719)

Size: px
Start display at page:

Download "JOHN F. BUTTS 8c ASSOC., INC. CONSULTING ENGINEERS 2480 VANTAGE DRIVE COLORADO SPRINGS, CO (719) FAX (719)"

Transcription

1

2

3 JOHN F. BUTTS 8c ASSOC., INC. CONSULTING ENGINEERS 2480 VANTAGE DRIVE COLORADO SPRINGS, CO (719) FAX (719) April 22, 1999 New Tech Machinery Corporation Street ~ Denver, CO Re: Panel Analysis Report New Tech SS 150 Panel New Tech SS210-A Panel New Tech SS550 Panel New Tech SS675 Panel JFBA Job NO Gentlemen: Per your request, we have completed an analysis of the above referenced panels. The panels, with the structural properties indicated in this report, is certified to meet or exceed the requirements of the following design specifications: American Iron and Steel Institute, Specifications for the Design of Cold-Formed Steel SfnrcrUral Members, 1996 edition. The following documents are enclosed for your records: Panel cross-section Panel analysis, pages 1 to 183 Panel Span Load tables, pages S1 to S71. Panels widths greater than 14 inches exceed the AISI allowable ratios for the panel width element. The AISI specifications, Section B 1.1 (a) states: J "... stiffened elements having w/t ratios larger than 500 can be used with adequate design strength to sustain the required loads; however; substantial deformations of such elements usually will invalidate the design equations of this specification."

4 Before using the enclosed panel span tables, you will need to review the analysis reports for each panel. It is our opinion that the panels with wlt ratio elements exceeding 500 should be verified by testing before using the respective panel spzn tables. Please note that the panel analysis and Load Tables have been evaluated based on the assumption that the proper bearing, side laps, end laps, bracing, anchorage and structural supports are being utilized in the member's installation. We do not certify the installation method, attachment and supporting materials. If you have any questions, please call or write the undersigned. Sincerely, President

5 NOTE: MATERIAL USAGE: 5 13/16" 12" - 24" + IMlERlAL LEIIGIII rltdlslt 22- ow EP $$ REV ECNNO. DATE RELEASED BY - r ~ r ~ ~ s.xx = f.ol.xxx = f.005 FRACTION = f 1/32" ANGLE = f 1/2' DRAY111 BY SAWYER DATE CH"Coy DATE NEW TECH MACHINERY COORP. PART ILK SIZE SC~LE SS200 PANEL PROFILE A NONE SHEEl PAW IIUUIJER 1 OF^ SS200 RRISILVI 0

6

7 PAGE NO. 3 7 Jshn F. Butts & Associates, Inc Vantage Drive Colorado Springs, CO (719) PROFILE ANALYSIS & DESIGN Per AISI Cold-Formed Steel Design Manual, 1996 Edition New Tech Panel FILE NAME: NT200 DIMENSIONS Line # 1 Angle Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius Length (R) = deg (R) = in (R) = in (R) = deg (R) = in (R) = 0.624in (R) = deg (R) = in (R) = in Line # 1 Angle Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius Length (L) = deg (L) = in (L) = in (L) = deg (L) = 0.040in (L) = in (L) = deg (L) = in (L) = in Panel Bottom Width = in Panel Overall Width = in Panel Overall Height= in Seam Rotation : 90 deg. Alloy: ASTM A653, G50 Fy = ksi Fv= 21.18ksi SPECIAL CONDITIONS QUALIFICATIONS PER AISI SPECIFICATIONS (a) Maximum w/t Ratio's Exceeded [SEC. Bl.l(a)] (b) Maximum h/t Ratio's Exceeded [SEC. B1.2(a)] No No PROPERTIES FOR LOAD/SPAN TABLES Aweb= in2 Sxp = in3 Sxp (per ft. of width) = in3 Sxn = in3 Sxn (per ft. of width) = in3 Ixp = in4 Ixp (per ft. of.width) = in4 Ixn = in4 Ixn (per ft. of width) = in4 Weight= 1.47 lb/lf

8 PAGE NO Member - Type Name Gage Hgt (in) Width (in) Lip (in) t (in) Weight lb/ft Coil Width (in) Panel PNL Gross Section Properties ~rea (in2) IX (in4) sx (in3) RX (in) YCg (in) IY (in4) SY (in3) RY (in) XCg (in) Effecti-ve Properties Ix (in4) Sx (in3) IY (in4) SY (in3) Mnx (in-k) (in-k) Vnx (kip) End Bearing Pne Pnei (kip) (k/in)' I Torsional Properties I 1 (E) 1 (?TI Beta Jv* 1000 E G (in4) [(~i;l ( ~ i )(ksi) 1 (%) (ksi) 1 Shear, moment and bearing values shown are nominal values and must be modified by the appropriate factors of safety (ASD) or resistance factors (LRFD). Factors of Safety (ASD) Resistance Factors (LRFD) R (Compression) = (Compression) = 0.85 R (Tension) = (Tension) = 0.95 R (Web Crippling) = (Web Crippling) = 0.75 R (Bending) = (Bending) = 1.11 R (Shear) = (Shear) = 0.90

9 PAGE NO Moment of 90 degree Rotation ELEMENT L Y LY LYY 10

10 PAGE NO. 40 LOAD ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY 10 Webs Fully Effective [SEC. B2.3(a)]l No

11 PAGE NO. 41 DEFLECTION ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY I0 Webs Fully Effective [SEC. B2-3 (a) ] 1 No

12 PAGE NO. 42 LOAD ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY I OQOO Webs Fully Effective [SEC. B2.3(a)]l No

13 PAGE NO. 43 New Tech Panel DEFLECTION ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY I0 Webs Fully Effective [SEC. B2.3(a) ] 1 Yes

14 PAGE NO. 44 MAXIMUM NOMINAL MOMENTS - [Section C3.1.l(a)] Mnx [positive bending] = k-in Mnx [negative bending] = k-in MAXIMUM ALLOWABLE REACTIONS - [Table C3.4-I.] N/t= k = C1 = C2 = C3 = C4 = C9 = CO = Element 2, 22 Pend= t^2*k*c3*c4*c9*co[ (h/t)][ (N/t)] h/t = Pe( 2)= kips = kips h/t = Pe(22)= 1 * kips = kips Pend= kips Pint= t^2*k*cl*c2*c9*c0[ (h/t)][ O.Oll(N/t)] h/t = Pi( 2)= 1 * kips = kips h/t = Pi(22)= 1 * kips = kips Pint= kips MAXIMUM NOMINAL SHEAR - [Section C3.21 E = 29,500 ksi Fy = ksi kv = for unreinforced webs 0,96O*Sqr(Ekv/Fy) = *Sqr (Ekv/Fy) = h/t = V( 2) = 1 * kips = kips (Eq. C3.2-2) h/t = V(22) = 1 * kips = kips (Eq. C3.2-2) Vn = kips

15 PAGE NO. 45 \ ============================================================================== '. Sheet Gauge = in, 24 gauge PANEL ELEMENTS EXCEEDING AISI ALLOWABLE RATIOS Element No. 14 : w/t>250 -Actual w/t = 495 NOTE: AISI Specifications, Section Bl.l(a) states....stiffened compression elements that have w/t ratios exceeding approximately 250 are likely to develop noticeable deformation at the full design strength, without affecting the ability of the mender to develop the required strength.

16 PAGE NO. 46 John F. Butts & Associates, Inc Vantage Drive Colorado Springs, CO (719) PROFILE ANALYSIS & DESIGN Per AISI Cold-Formed Steel Design Manual, 1996 Edition FILE NAME: NT200 DIMENSIONS Line # 1 Angle Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius Length (R) = deg (R) = in (R) = in (R) = deg (R) = in (R) = in (R) = deg (R) = in (R) = in Line # 1 Angle Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius ' Length (L) = deg (L) = 0.040in (L) = in (L) = deg (L) = in (L) = in (L) = deg (L)= 0.040in (L) = in Panel Bottom Width = in Panel Overall Width = in Panel Overall Height= in Seam Rotation : 90 deg. Alloy: ASTM A653, G50 Fy = ksi Fv= 21.18ksi SPECIAL CONDITIONS QUALIFICATIONS PER AISI SPECIFICATIONS (a) Maximum w/t Ratio's Exceeded [SEC. (b) Maximum h/t Ratio's Exceeded (SEC. : 1 No PROPERTIES FOR LOAD/SPAN TABLES Aweb= in2 Sxp = in3 Sxp (per ft. of width) = in3 Sxn = in3 Sxn (per ft. of width) = in3 Ixp = in4 Ixp (per ft. of width) = in4 Ixn = in4 Ixn (per ft. of width) = in4 Weight= 1.63 lb/lf No

17 PAGE NO. 47 New Tech Panel Member - Type Name Gage Hgt (in) Width (in) Lip (in) t (in) Weight lb/ft Coil Width (in) Panel PNL I Gross Section Properties I Area (in2) Ix (in4) 24 Sx (in3) Rx (in) YCg (in) 0,000 IY (in4) SY (in3) RY (in) XCg ( in) Ef f ectkve Properties - - Ix (in4) Sx (in3) IY (in4) SY (in3) Mnx (in-k) MnY (in-k) Vnx (kip) End Bearing Pne Pnei (kip) (k/in) Torsional Properties Xo (in) Ro (in) Beta Cw (in6) Jv*1000 (in4) Fy (ksi) Fu (ksi) E (ksi) G (ksi) Shear, moment and bearing values shown are nominal values and must be modified by the appropriate factors of safety (ASD) or resistance factors (LRFD). Factors of Safety (ASD) Resistance Factors (LRFD) R (Compression) = 1.80 $J (Compression) = 0.85 R (Tension) = 1.67 $J (Tension) = 0.95 R (Web Crippling) = 1.85 $J (Web Crippling) = 0.75 R (Bending) = 1.67 $J (Bending) = 1.11 R (Shear) = 1.67 $J (Shear) = 0.90

18 PAGE NO. 48 Moment of 90 degree Rotation ELEMENT L Y LY LYY 10

19 PAGE NO. 49 New Tech Panel LOAD ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY I0 Webs Fully Effective [SEC. B2.3(a)] 1 No

20 PAGE NO. 50 New Tech Panel DEFLECT ION ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY 10 Webs Fully Effective [SEC. B2.3(a)] 1 No

21 PAGE NO. 51 LOAD ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY 10 Webs Fully Effective [SEC. B2.3(a)]l No

22 PAGE NO. 52 DEFLECTION ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY I0 Webs F ully Effective. [SEC. B2.3(a)] 1 Yes

23 PAGE NO. 53 MAXIMUM NOMINAL MOMENTS - [Section C3.1.l(a)] ~ n x [positive bending] = mx [negative bending] = k-in k-in MAXIMUM ALLOWABLE =ACTIONS - [Table C N/t= k = Cl = C2 = C3 = C4 = C9 = CO = Element Pend= t^2*k*c3*c4*c9*c0[ (h/t)][ (N/t)] h/t = Pe( 2)= 1 * kips = kips h/t = Pe(22)= 1 * kips = kips Pend= kips Pint= ta2*k*c1*c2*c9*c0[ (h/t)][ O.Oll(N/t)] h/t = Pi( 2)= 1 * kips = kips. h/t = Pi(22)= 1 * kips = kips Pint= kips MAXIMUM NOMINAL SHEAR - [Section C3.21 E = 29,500 ksi Fy = ksi kv = for unreinforced webs 0.960*sqr(Ekv/Fy) = *Sqr(Ekv/Fy) = h/t = V( 2) = 1 * kips = kips (Eq. C3.2-2) h/t = V(22) = 1 * 1.,035 kips = kips (Eq. C3.2-2) Vn = kips

24 PAGE NO. 54 Sheet Gauge = in, 24 gauge PANEL ELEMENTS EXCEEDING AISI ALLOWABLE RATIOS Element No. 14 : w/t>500 -Actual w/t = 578 NOTE: AISI Specifications, Section Bl.l(a) states.... stiffened elements having w/t ratios larger than 500 can be used with adequate design strength to sustain the required loads; however; substantial deformations of such elements usually will invalidate the design equations of this Specification.

25 PAGE NO. 55 John F. Butts & Associates, Inc Vantage Drive Colorado Springs, CO (719) PROFILE ANALYSIS & DESIGN Per AISI Cold-Formed Steel Design Manual, 1996 Edition FILE NAME: NT200 DIMENSIONS Line # 1 Angle Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius Length (R) = deg (R) = in (R) = in (R) = deg (R) = in (R) = in (R) = deg (R) = in (R) = in Line # 1 Angle. Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius Length (L) = deg (L)= 0.040in (L) = in (L) = deg (L) = in (L) = in (L) = deg (L) = in (L) = in Panel Bottom Width = in Panel Overall Width = in Panel Overall Height= in Seam Rotation : 90 deg. Alloy: ASTM A653, 650 Fy = ksi ' Fv= ksi SPECIAL CONDITIONS QUALIFICATIONS PER AISI SPECIFICATIONS (a) Maximum w/t Ratio's Exceeded [SEC. (b) Haximum h/t Ratio's Exceeded [SEC. : 1 No PROPERTIES FOR LOAD/SPAN TABLES Aweb= in2 Sxp = in3 Sxp (per ft. of width) = in3 Sxn = in3 Sxn (per ft. of width) = in3 Ixp = in4 Ixp (per ft. of width) = in4 Ixn = in4 Ixn (per ft. of width) = in4 Weight= 1.80 lb/lf No

26 PAGE NO. 56 Member - Type Name Gage Hgt (in) Width (in) Lip (in) t (in) Weight lb/ft Coil Width (in) Panel PNL Gross Section Properties Area (in2) Ix (in4) Sx (in3) Rx (in). YCg (in) IY (in4) SY (in3) RY (in) XCg (in) Effective Properties I x (in4) Sx (in3) IY (in4) SY (in3) Mnx (in-k) MnY (in-k) Vnx (kip) End Bearing Pne Pnei (kip) (k/in) Torsional Properties Xo (in) Ro (in) Beta Cw (in6) Jv*1000 (in4) Fy (ksi) Fu (ksi) E (ksi) G (ksi) Shear, moment and bearing values shown are nominal values and must be modified by the appropriate factors of safety (ASD) or resistance factors (LRFD). Factors of Safety (ASD) Resistance Factors (LRFD) R (Compression) = 1.80 (Compression) = 0.85 R (Tension) = 1.67 (Tension) = 0.95 R (Web Crippling) = (Web Crippling) = 0.75 R (Bending) = (Bending) = 1.11 R (Shear) = (Shear) = 0.90

27 PAGE NO. 57 Moment of 90 degree Rotation ELEMENT L Y LY LYY 10

28 PAGE NO. 58 LOAD ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY 10 Webs F ully Effective [SEC. B2.3(a)]) No

29 PAGE NO. 59 DEFLECTION ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY I0 Webs Fully Effective [SEC. B2.3 (a) 1 1 No

30 PAGE NO. 60 LOAD ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY I0 Webs Fully Effective [SEC. B2.3 (a)] 1 No

31 PAGE NO. 61 DEFLECTION ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY I0 Webs Fully Effective [SEC. B2.3(a)]( Yes

32 PAGE NO. 62 New Tech Panel MAXIMUM NOMINAL MOMENTS - [Section C3.1.l(a)] Mnx [positive bending] = k-in a x [negative bending] = k-in MAXIMUM ALLOWABLE REACTIONS - [Table C N/t= k = C-l = C2 = C3 = C4 = C9 = CO = Element (h/t)][ (N/t)] Pend= t^2*k*~3*~4*~9*~0[217 h/t = Pe( 2)= 1 * kips = kips h/t = Pe(22)= 1 * kips = kips Pend= kips Pint= ta2*k*c1*c2*c9*c0 [ (h/t) 1 [ (N/t) ] h/t = Pi( 2)= 1 * kips = kips h/t = Pi(22)= 1 * kips = kips Pint= kips MAXIMUM NOMINAL SHEAR - [Section C3.21 E = 29,500 ksi Fy = ksi kv = for unreinforced webs 0,96O*Sqr(Ekv/Fy) = *Sqr(Ekv/Fy) = h/t = V( 2) = 1 * kips = kips (Eq. C3.2-2) h/t = V(22) = 1 * kips = kips (Eq. C3.2-2) Vn = kips

33 PAGE NO. 63 New Tech Panel Sheet Gauge = in, 24 gauge PANEL ELEMENTS EXCEEDING AISI ALLOWABLE RATIOS Element No. 14 : w/t>500 -Actual w/t = 661 NOTE: AISI Specifications, Section Bl.l(a) states... stiffened elements having w/t ratios larger than 500 can be used with adequate design strength to sustain the required loads; however! substantial deformations of such elements usually will invalidate the design equations of this Specification.

34 PAGE NO. 64 John F. Butts 8 Associates, Inc Vantage Drive Colorado Springs, CO (719) PROFILE ANALYSIS & DESIGN Per AISI Cold-Formed Steel Design Manual, 1996 Edition FILE NAME: NT200 DIMENSIONS Line # 1 Angle Radius Length Line # 2 Anqle Radius Length Line # 3 Angle Radius Length (R) = deg (R) = in (R) =.l.872 in (R) = deg (R) = in (R) = in (R) = deg (R) = in (R) = in Line # 1 Angle Radius Length Line # 2 Angle Radius Length Line # 3 Angle Radius Length (L) = deg (L) = in (L) = in (L) = deg (L) = in (L) = in (L) = deg (L) = in (L)= 0.669in Panel Bottom Width = in Panel Overall Width = in Panel Overall Height= in Seam Rotation : 90 deg. Alloy: ASTM A653, 650 Fy = ksi Fv = ksi SPECIAL CONDITIONS QUALIFICATIONS PER AISI SPECIFICATIONS (a) Maximum w/t Ratio's Exceeded [SEC. Bl.l(a)] (b) Maximum h/t Ratio's Exceeded [SEC. B1.2(a)] PROPERTIES FOR LOAD/SPAN TABLES Aweb= in2 Sxp = in3 Sxp (per ft. of width) = in3 Sxn = in3 Sxn (per ft. of width) = in3 Ixp = in4 Ixp (per ft. of width) = in4 Ixn = in4 Ixn (per ft. of width) = in4 Weight= 1.96 lb/lf

35 PAGE NO. 65 New Tech Panel Member - New Tech Panel Type Name Gage Hgt Width Lip t Weight Coil Width (in) (in) (in) (in) lb/ft Panel PNL Area Ix Sx Rx Gross Section Properties Ix (in4) Sx (in3) IY (in4) SY (in3) Mnx (in-k) MnY (in-k) Vnx (kip) End Bearing Pne Pne i (kip) (k/in) Torsional Properties Xo (in) Ro (in) Beta Cw (in6) Jv*1000 (in4) Fy (ksi) Fu (ksi) E (ksi) G (ksi) Shear, moment and bearing values shown are nominal values and must be modified by the appropriate factors of safety (ASD) or resistance factors (LRFD). Factors of Safety (ASD) Resistance Factors (LRFD) R (Compression) = (Compression) = 0.85 R (Tension) = 1.67 (Tension) = 0.95 R (Web Crippling) = (Web Crippling) = 0.75 R (Bending) = (Bending) = 1.11 R (Shear) = (Shear) = 0.90

36 PAGE NO. 66 Moment of 90 degree Rotation ELEMENT L Y LY LYY 10

37 PAGE NO. 67 LOAD ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY 10 Webs F ully Effective [SEC. B2.3(a)]l No

38 PAGE NO. 68 DEFLECTION ELEMENT VALUES FOR POSITIVE BENDING ELEMENT L Y LY LYY 10 Webs Fully E ffective [SEC. B2.3(a) ] 1 No

39 PAGE NO. 69 LOAD ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY 10 Webs Fully Effective [SEC. B2.3(a) ] 1 No

40 PAGE NO. 70 New Tech Panel DEFLECTION ELEMENT VALUES FOR NEGATIVE BENDING ELEMENT L Y LY LYY 10 Webs Fully Effective [SEC. B2.3(a)]l Yes

41 PAGE NO. 71 MAXIMUM NOMINAL MOMENTS - [Section C3.1.l(a)] Mnx [positive bending] = k-in Mnx [negative bending] = k-in MAXIMUM ALLOWABLE REACTIONS - [Table C N/t= k = Cl = C2 = C3 = C4 = C9 = CO = Element 2, 22 Pend= t^2*k*c3*c4*c9*c0[ (h/t)][ (N/t)] h/t = Pe( 2)= 1 * kips = kips h/t = Pe(22)= 1 * kips = kips Pend= kips Pint= t^2*k*cl*c2*c9*c0[ (h/t)][ O.Oll(N/t)] h/t = Pi( 2)= 1 * kips = kips h/t = Pi(22)= 1 * kips = kips Pint= kips MAXIMUM NOMINAL SHEAR - [Section C3.21 E = 29,500 ksi Fy = ksi kv = for unreinforced webs 0.960*Sqr(Ekv/Fy) = *Sqr(Ekv/Fy) = h/t = V( 2) = 1 * kips = kips (Eq. C3.2-2) h/t = V(22) = 1 * kips = kips (Eq. C3.2-2) Vn = kips

42 PAGE NO. 72 Sheet Gauge = in, 24 gauge PANEL ELEMENTS EXCEEDING AISI ALLOWABLE RATIOS Element No. 14 : w/t>500 -Actual w/t = 745 NOTE: AISI Specifications, Section Bl.l(a) states... stiffened elements having w/t ratios larger than 500 can be used with adequate design strength to sustain the required loads; however; substantial deformations of such elements usually will invalidate the design equations of this Specification.

43

44

45 PAGE NO. S13 - c Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 SPAN DEFLECTION ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn=.125w12, x=.0130w1^4/ei Two Span Mp=.125w12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp=.080wl2, Mn=.107w12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 Q (Shear) = 1.67 Q (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

46 PAGE NO. S14 Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn=.125w12, x=.0130wla4/ei Two Span ~ p =.125w12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp= -080~12, Mn=.107w12, x=.0069wla4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: $2 (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) TWO Span : Max. Span = ft (L/180) Three Span +: Max. Span = 9,418 ft (L/180)

47 PAGE NO. S15 Width Alloy Gauge in ASTM A653, G50 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN DEFLECTION SPAN LENGTH (Feet) L/ L/ L/ Formula's u,sed in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn= -125~12, x=.0130w1^4/ei Two Span - Mp=.125w12, Mn= -096~12, x=.0092wla4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069w1'4/ei Modulas of Elasticity (E) = 29,500 ksi. 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) TWO Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

48 PAGE NO. S16 Width Alloy Gauge 12.OO in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn=.125w12, x=.0130w1'4/ei Two Span Mp= -125~12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp= -080~12, Mn=.107w12, x=.0069w1'4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.2) b) Combined Bending and Shear [AISI C3.3) c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) TWO Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

49 PAGE NO- 517 Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD.(PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn= -125~12, x=.0130w1^4/ei Two Span ~ p =.125w12, Mn= -096~12, x= -0092~1-4/,EI Three Span - Mp=.080wl2, Mn= -107~12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Benaing and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

50 PAGE NO. S18 Width Alloy Gauge in ASTM A653, G50 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN DEFLECTION SPAN LENGTH (Feet) J Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn=.125w12, x=.0130w1^4/ei Two Span Mp=.125w12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp=.080wl2, Mn=.107wlz, x=.0069w1'4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

51 PAGE NO. S19 New Tech Panel Width Alloy Gauge in ASTM A653, G50 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn=.125wl2, x=,0130~1-4/ei Two Span Mp= -125~12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp= -080~12, Mn=.107w12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max, Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

52 PAGE NO. S20 Width Alloy Gauge in ASTM A653, G5O (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn= -125~12, x=.0130w1^4/ei Two Span Mp= -125~12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp= -080~12, Mn= -107~12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) TWO Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

53 PAGE NO. S21 New Tech ss200 Panel Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. - SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn= -125~12, x=.0130wla4/ei Two Span Mp=.125w12, Mn=.096w12, x=.0092wla4/ei Three Span - Mp= -080~12, Mn=.107wl2, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads:, R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = it (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = it (L/180)

54 PAGE NO. S22 Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. New Tech. SSZOO Panel SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1-0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's,used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn=.125w12, x=.013gw1^4/ei Two Span Mp= -125~12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069wla4/ei Modulas of Elasticity (E) = 29,500 ksi. 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

55 PAGE NO. S23 Width Alloy Gauge in ASTMA653, G50 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn= -125~12, x=.0130w1^4/ei Two Span Mp=.125w12, Mn=.096w12, x=.0092w1'4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069w1'4/ei Modulas of Elasticity (.E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

56 PAGE NO. S24 SPAN DEFLECTION Width Alloy Gauge in ASTM A653, G50 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn=.125w12, x=.0130w1^4/ei Two Span Mp=.125w12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp=.080w12, Mn=.107wlz, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 C) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads:. R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

57 PAGE NO. S25 Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn= -125~12, x=.0130w1^4/ei Two Span Mp=.125w12, Mn=.096w12, x=.0092w1'4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

58 PAGE NO. S26 New Tech Panel Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION - =LOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp= -125~12, Mn=.125w12, x=.0130w1^4/ei Two Span Mp= -125~12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069wla4/ei Modulas of Elasticity /E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = it (L/180) Two span : Max. Span = ft (L/180) Three Span +: Max. Span = it (L/180)

59 PAGE NO. S27 Width Alloy Gauge in ASTM A653, 650 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. ALLOWABLE STRENGTH DESIGN (ASD) '7 Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN DEFLECTION SPAN LENGTH (Feet) 1. Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn=.125w12, x=.0130w1^4/ei Two Span Mp= -125~12, Mn=.096w12, x=.0092w1^4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1.67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

60 PAGE NO. S28 Width Alloy Gauge in ASTM A653, G50 (Fy= 50 ksi) 24 (0.024 in) Seam Rotation : 90 deg. SPAN DEFLECTION ALLOWABLE STRENGTH DESIGN (ASD) Wind Load Factor = 1.0 ALLOWABLE UNIFORM LOAD (PSF) SPAN LENGTH (Feet) 1..Formula's used in Load Tables for FLEXURE and DEFLECTION are: One Span Mp=.125w12, Mn=,125~12, x=.0130w1^4/ei Two Span Mp=.125w12, Mn= -096~12, x=.0092w1^4/ei Three Span - Mp=.080w12, Mn=.107w12, x=.0069w1^4/ei Modulas of Elasticity (E) = 29,500 ksi 2. Allowable uniform loads are determined per the following: a) Allowable Shear Stress (Fv) [AISI C3.21 b) Combined Bending and Shear [AISI C3.31 c) Combined Bending & Web Crippling [AISI C Factors of Safety used to determine uniform loads: R (Bending) = 1.67 R (Shear) = 1i67 R (Web Crippling) = Allowance has been made for member Dead Weight. 5. Minimum panel support bearing length = 2.00 in 6. Concentrated load = 150 lb at mid-span, load width = 4 in Simple Span : Max. Span = ft (L/180) Two Span : Max. Span = ft (L/180) Three Span +: Max. Span = ft (L/180)

61

62

CHECK STRESS ON DECK BASED ON SDI REQUIREMENTS

CHECK STRESS ON DECK BASED ON SDI REQUIREMENTS ANALYSIS OF NON-COMPOSITE CONCRETE SLAB ON METAL DECK Lab #7 Question #2 A 6" total depth lightweight concrete slab with compressive strength of 3000psi is placed simply supported on a galvanized steel

More information

ANALYSIS OF COMPOSITE CONCRETE SLAB ON METAL DECK

ANALYSIS OF COMPOSITE CONCRETE SLAB ON METAL DECK ANALYSIS OF COMPOSITE CONCRETE SLAB ON METAL DECK Assignment #5 Select a Vulcraft composite deck to support 150 psf service live load on a 10 ft clear span. The steel deck is to be used on a three-span

More information

Finite Element Analysis of a 10 x 22 FRP Building for TRACOM Corporation

Finite Element Analysis of a 10 x 22 FRP Building for TRACOM Corporation Finite Element Analysis of a 10 x 22 FRP Building for TRACOM Corporation May 29, 2007 A. Background TRACOM Corporation designs and constructs Fiber Reinforced Plastic Buildings for use as shelters around

More information

Important Note - Please Read:

Important Note - Please Read: Important Note - Please Read: This tutorial requires version 6.01 or later of SAFE to run successfully. You can determine what version of SAFE you have by starting the program and then clicking the Help

More information

Southwest Windpower Inc. Doc. # Southwest Windpower Inc. 27 Air Tower Analysis 7/7/03

Southwest Windpower Inc. Doc. # Southwest Windpower Inc. 27 Air Tower Analysis 7/7/03 Southwest Windpower Inc. Doc. # 0185 Southwest Windpower Inc. 27 Air Tower Analysis 7/7/03 1. Introduction: The following analysis covers tower stress and anchor loads for the Southwest Wndpower 27' Air

More information

PENNDOT e-notification Bureau of Business Solutions and Services Highway/Engineering Application Division

PENNDOT e-notification Bureau of Business Solutions and Services Highway/Engineering Application Division PENNDOT e-notification Bureau of Business Solutions and Services Highway/Engineering Application Division STLRFD No. 009 August 27, 2012 Release of Version 2.1.0.0 The Department s LRFD Steel Girder Design

More information

Problem 1. Lab #12 Solution

Problem 1. Lab #12 Solution Lab #1 Solution Problem 1 Given Truss Roof Dead Load of 16 psf, Snow Live load of 16 psf, Truss spacing of 4" o.c. Lumber is No. DF-L Bolt holes are 7/" diameter, MC < 19%, Temp < 100 degree F, and Ci

More information

Earthbound Welded Anchor Calculations

Earthbound Welded Anchor Calculations Earthbound Welded Anchor Calculations Objective: Find a welded anchor to steel beam connection able to handle 1.125 inch diameter A193B7 Threaded. Calculate the welding requirements for welding a round

More information

FB-MULTIPIER vs ADINA VALIDATION MODELING

FB-MULTIPIER vs ADINA VALIDATION MODELING FB-MULTIPIER vs ADINA VALIDATION MODELING 1. INTRODUCTION 1.1 Purpose of FB-MultiPier Validation testing Performing validation of structural analysis software delineates the capabilities and limitations

More information

ADAPT-PT/RC 2018 Getting Started Tutorial ADAPT-RC mode

ADAPT-PT/RC 2018 Getting Started Tutorial ADAPT-RC mode ADAPT-PT/RC 2018 Getting Started Tutorial ADAPT-RC mode Update: September 2018 Copyright ADAPT Corporation all rights reserved ADAPT-PT/RC 2017-Tutorial- 1 This ADAPT-PT/RC 2018 Getting Started Tutorial

More information

cover to the center of the bars depth of bottom reinforcement (h cover) depth of top reinforcement (h cover)

cover to the center of the bars depth of bottom reinforcement (h cover) depth of top reinforcement (h cover) Interaction (ACI318) Checker today Input Column dimensions Reinforcement Materials (steel, concrete, bolts) Output Moment capacity Column interaction diagram RC Column Capacity - Axial Force - Bending

More information

Important Note - Please Read:

Important Note - Please Read: Important Note - Please Read: This tutorial requires version 6.01 or later of SAFE to run successfully. You can determine what version of SAFE you have by starting the program and then clicking the Help

More information

17. SEISMIC ANALYSIS MODELING TO SATISFY BUILDING CODES

17. SEISMIC ANALYSIS MODELING TO SATISFY BUILDING CODES 17. SEISMIC ANALYSIS MODELING TO SATISFY BUILDING CODES The Current Building Codes Use the Terminology: Principal Direction without a Unique Definition 17.1 INTRODUCTION { XE "Building Codes" }Currently

More information

1.2 Connection configurations:

1.2 Connection configurations: 1.2 Connection configurations: 1.2.1 Simple connections: Simple connections are assumed to transfer shear only shear at some nominal eccentricity. Therefore such connections can be used only in non-sway

More information

Three- Span Continuous Horizontally Curved. Composite Steel TUB Girder Bridge

Three- Span Continuous Horizontally Curved. Composite Steel TUB Girder Bridge Three- Span Continuous Horizontally Curved Composite Steel TUB Girder Bridge WIZARD, ANALYSIS AND DESIGN TUB Girder Curved Contents Bridge Information Material and Section Properties Wizard Modelling Tweaks

More information

This is NOT a truss, this is a frame, consisting of beam elements. This changes several things

This is NOT a truss, this is a frame, consisting of beam elements. This changes several things CES 44 - Stress Analysis Spring 999 Ex. #, the following -D frame is to be analyzed using Sstan (read the online stan intro first, and Ch-6 in Hoit) 5 k 9 E= 9000 ksi 8 I= 600 in*in*in*in 5 A= 0 in*in

More information

RISA 3D. Verification Problems. Rapid Interactive Structural Analysis 3 Dimensional

RISA 3D. Verification Problems. Rapid Interactive Structural Analysis 3 Dimensional RISA 3D Rapid Interactive Structural Analysis 3 Dimensional Verification Problems 26632 Towne Centre Drive, Suite 210 Foothill Ranch, California 92610 (949) 951 5815 (949) 951 5848 (FAX) www.risatech.com

More information

CONCRETE DESIGN SOFTWARE LIBRARY

CONCRETE DESIGN SOFTWARE LIBRARY CONCRETE DESIGN SOFTWARE LIBRARY DESIGN AND INVESTIGATION OF REINFORCED CONCRETE CONTINUOUS BEAMS PORTLAND CEMENT ASSOCIATION 5420 Old Orchard Road, Skokie, Illinois 60077-1083 Telephone: (847) 966-4357

More information

AISIBEAM User's Manual (Version 3.0)

AISIBEAM User's Manual (Version 3.0) AISIBEAM User's Manual (Version 3.0) Shabin Taavoni, Ph.D., PE, title Structural Software Inc. location John C. Huang Ph.D., PE, Principal CHC Engineering, LLC Herndon, VA Scope of Software The software

More information

ADAPT-PT/RC 2014 Getting Started Tutorial ADAPT-RC mode

ADAPT-PT/RC 2014 Getting Started Tutorial ADAPT-RC mode ADAPT-PT/RC 2014 Getting Started Tutorial ADAPT-RC mode Update: January 2014 Copyright ADAPT Corporation all rights reserved ADAPT-PT/RC 2014-Tutorial- 1 This ADAPT-PT/RC 2014 Getting Started Tutorial

More information

midas Civil Advanced Webinar Date: February 9th, 2012 Topic: General Use of midas Civil Presenter: Abhishek Das Bridging Your Innovations to Realities

midas Civil Advanced Webinar Date: February 9th, 2012 Topic: General Use of midas Civil Presenter: Abhishek Das Bridging Your Innovations to Realities Advanced Webinar Date: February 9th, 2012 Topic: General Use of midas Civil Presenter: Abhishek Das Contents: Overview Modeling Boundary Conditions Loading Analysis Results Design and Misc. Introduction

More information

PennDOT e-notification Bureau of Business Solutions and Services Highway/Engineering Applications Division

PennDOT e-notification Bureau of Business Solutions and Services Highway/Engineering Applications Division PennDOT e-notification Bureau of Business Solutions and Services Highway/Engineering Applications Division STLRFD No. 013 October 17, 2016 Release of Version 2.4.0.0 The Department s LRFD Steel Girder

More information

Application nr. 2 (Global Analysis) Effects of deformed geometry of the structures. Structural stability of frames. Sway frames and non-sway frames.

Application nr. 2 (Global Analysis) Effects of deformed geometry of the structures. Structural stability of frames. Sway frames and non-sway frames. Application nr. 2 (Global Analysis) Effects of deformed geometry of the structures. Structural stability of frames. Sway frames and non-sway frames. Object of study: multistorey structure (SAP 2000 Nonlinear)

More information

Ansys Lab Frame Analysis

Ansys Lab Frame Analysis Ansys Lab Frame Analysis Analyze the highway overpass frame shown in Figure. The main horizontal beam is W24x162 (area = 47.7 in 2, moment of inertia = 5170 in 4, height = 25 in). The inclined members

More information

Hilti North America Installation Technical Manual Technical Data MI System Version

Hilti North America Installation Technical Manual Technical Data MI System Version MIC-CU-MAH 2174664 Hilti North America Installation Technical Manual Technical Data MI System Version 1.2 08.2017 Terms of common cooperation / Legal disclaimer The product technical data published in

More information

Idealization of Design Strip in ADAPT RC

Idealization of Design Strip in ADAPT RC ADAPT RC 2010 Tutorial Idealization of Design Strip in ADAPT RC Update: May 2010 Copyright ADAPT Corporation all rights reserved ADAPT RC 2010 Tutorial 1 Main Toolbar Menu Bar View Toolbar Structure View

More information

AASHTOWare BrR - SIMPLE SPAN PRESTRESSED I BEAM EXAMPLE - BR 76015

AASHTOWare BrR - SIMPLE SPAN PRESTRESSED I BEAM EXAMPLE - BR 76015 AASHTOWare BrR - SIMPLE SPAN PRESTRESSED I BEAM EXAMPLE - BR 76015 M N D O T B R I D G E S T A T E A I D Page 1 PS1 - Simple Span Prestressed I Beam Example (BrR 6.7.1) 1. From the Bridge Explorer create

More information

Case Study - Vierendeel Frame Part of Chapter 12 from: MacLeod I A (2005) Modern Structural Analysis, ICE Publishing

Case Study - Vierendeel Frame Part of Chapter 12 from: MacLeod I A (2005) Modern Structural Analysis, ICE Publishing Case Study - Vierendeel Frame Part of Chapter 1 from: MacLeod I A (005) Modern Structural Analysis, ICE Publishing Iain A MacLeod Contents Contents... 1 1.1 Vierendeel frame... 1 1.1.1 General... 1 1.1.

More information

North US 290 US 183. MLK Blvd. FM 969. ASERO Steel Sales. Ben White TX 71 IH-35 US 183

North US 290 US 183. MLK Blvd. FM 969. ASERO Steel Sales. Ben White TX 71 IH-35 US 183 North US 290 US 8 MLK Blvd. FM 969 ASERO Steel Sales Ben White TX IH- US 8 Hot Rolled Strip Commercial Quality A - 0 Size in Per 20 Ft. /8 x /2.2 4.26 /4.9 6.8.42 8.0 /4. 0.62 /2.68 2.6 2.80.00 2 /2.06

More information

= 21

= 21 CE 331, Spring 2011 Guide for Using RISA3D to Model a Balsa Structure 1 / 9 0. Example Bridge. An example structure is shown below. Typical results for the RISA model of this structure are shown throughout

More information

STRENX TUBE 100XF STRENX TUBE 100XF. General Product Description

STRENX TUBE 100XF STRENX TUBE 100XF. General Product Description STRENX TUBE 100XF STRENX TUBE 100XF General Product Description Advanced high-strength structural hollow sections Strenx Tube 100XF is an HF-welded cold-formed structural hollow section made of hot-rolled

More information

Chapter 3 Analysis of Original Steel Post

Chapter 3 Analysis of Original Steel Post Chapter 3. Analysis of original steel post 35 Chapter 3 Analysis of Original Steel Post This type of post is a real functioning structure. It is in service throughout the rail network of Spain as part

More information

D DAVID PUBLISHING. Stability Analysis of Tubular Steel Shores. 1. Introduction

D DAVID PUBLISHING. Stability Analysis of Tubular Steel Shores. 1. Introduction Journal of Civil Engineering and Architecture 1 (216) 563-567 doi: 1.17265/1934-7359/216.5.5 D DAVID PUBLISHING Fábio André Frutuoso Lopes, Fernando Artur Nogueira Silva, Romilde Almeida de Oliveira and

More information

Beam Data mp := 10. Beam length (ft) = length := Composite slab strength (psi) = fc := 4. Concrete unit weitht (kcf) = γc := 0.

Beam Data mp := 10. Beam length (ft) = length := Composite slab strength (psi) = fc := 4. Concrete unit weitht (kcf) = γc := 0. LRFD sla negative moment.mcd 7/1/3 1 of 3 Beam Data mp := 1 Beam length (ft) = length := 77. Composite sla strength (psi) = fc := 4 Concrete unit weitht (kcf) = γc :=.15 Initial strength of concrete (ksi)

More information

TILBURY STEEL SERVICE CENTRE

TILBURY STEEL SERVICE CENTRE TILBURY STEEL SERVICE CENTRE 159 Queen Street North Tilbury, ON, N0P 2L0 Voice: 519-682-0000 Toll-Free: 1-800-565-1077 Fax: 519-682-0004 Email: tsales@tilburysteel.com STOCK BOOK & REFERENCE GUIDE Tilbury

More information

Shear and Moment Diagram on a Simply Supported Flexural member

Shear and Moment Diagram on a Simply Supported Flexural member Shear and Moment Diagram on a Simply Supported Fleural member Eercise announcement: Construct a shear and moment diagram to analyze the element indicated below. Data Preparation: It is noted that a non

More information

= Set the units Click on the units icon, and change the default units to lbs and inches for:

= Set the units Click on the units icon, and change the default units to lbs and inches for: CE 331, Fall 2012 Guide for Using RISA3D to Model a Balsa Structure 1 / 9 Example Bridge. An example structure is shown below. Typical results for the RISA model of this structure are shown throughout

More information

UNIT III KANI S METHOD

UNIT III KANI S METHOD SIDDHARTH GROUP OF INSTITUTIONS :: PUTTUR Siddharth Nagar, Narayanavanam Road 517583 QUESTION BANK (DESCRIPTIVE) Subject with Code : SA-II (13A01505) Year & Sem: III-B.Tech & I-Sem Course & Branch: B.Tech

More information

SAP 2000 Problem II Homework Problem P5.45. Recall from Lab #6 the Global and Local Reference Coordinate Systems for 2D Problems

SAP 2000 Problem II Homework Problem P5.45. Recall from Lab #6 the Global and Local Reference Coordinate Systems for 2D Problems SAP 2000 Problem II Homework Problem P5.45 Recall from Lab #6 the Global and Local Reference Coordinate Systems for 2D Problems Z 2 Global (XYZ) Coordinate System Joint Displacements Applied Point Loads

More information

ST5 - Weld Design. FRILO Software GmbH as of

ST5 - Weld Design. FRILO Software GmbH   as of ST5 - Weld Design FRILO Software GmbH www.frilo.com info@frilo.com as of 29.03.2016 ST5 ST5 Weld Design Contents Application options 4 Basis of calculation 4 Verification of welding seams 4 Constructive

More information

Frame Analysis Using Multiframe4D

Frame Analysis Using Multiframe4D Frame Analysis Using Multiframe4D 1. The software is on the computers in the college computing lab (http://thelab.tamu.edu) in Programs under the Windows Start menu. Multiframe4D is under the COSC menu.

More information

SCH 5S/10S/40S/80S. Stainless Steel/Carbon Steel Butt-welding Fittings

SCH 5S/10S/40S/80S. Stainless Steel/Carbon Steel Butt-welding Fittings Stainless Steel/arbon Steel Butt-welding Fittings SH 5S/10S/40S/80S Ranged from equal and reduced tees, 45 and 90 elbows, concentric and eccentric reducers, to stub ends and caps, DIE ERSTE supplies a

More information

1. Define the material properties. Activate the Data Entry menu if it s not already visible, and click on Materials.

1. Define the material properties. Activate the Data Entry menu if it s not already visible, and click on Materials. CE 533, Fall 2014 Guide for Using RISA3D 1 / 9 Example Structure. The procedure for calculating frequencies and modes shapes of a multidegree of freedom (MDOF) system will be demonstrated using the following

More information

COMMONWEALTH OF PENNSYLVANIA DEPARTMENT OF TRANSPORTATION

COMMONWEALTH OF PENNSYLVANIA DEPARTMENT OF TRANSPORTATION COMMONWEALTH OF PENNSYLVANIA DEPARTMENT OF TRANSPORTATION www.dot.state.pa.us DATE: September 23, 2002 SUBJECT: TO: FROM: LRFD Prestressed Concrete Girder Design and Rating PSLRFD Version 2.0 District

More information

Manual BS : 2000 steel code check

Manual BS : 2000 steel code check Manual BS 5950-1: 2000 steel code check 1 All information in this document is subject to modification without prior notice. No part or this manual may be reproduced, stored in a database or retrieval system

More information

SIDDHARTH GROUP OF INSTITUTIONS :: PUTTUR Siddharth Nagar, Narayanavanam Road QUESTION BANK (DESCRIPTIVE) UNIT I ARCHES

SIDDHARTH GROUP OF INSTITUTIONS :: PUTTUR Siddharth Nagar, Narayanavanam Road QUESTION BANK (DESCRIPTIVE) UNIT I ARCHES SIDDHARTH GROUP OF INSTITUTIONS :: PUTTUR Siddharth Nagar, Narayanavanam Road 517583 QUESTION BANK (DESCRIPTIVE) Subject with Code : SA-II (13A01505) Year & Sem: III-B.Tech & I-Sem Course & Branch: B.Tech

More information

Exam 1 Problem #1. Exam Solution - Problem #1. Given information. Temperatures. Thermal Resistance

Exam 1 Problem #1. Exam Solution - Problem #1. Given information. Temperatures. Thermal Resistance Exam 1 Problem #1 Calculate the coefficient of thermal transmittance, U, and the thermal gradient through the wall. Exam Solution - Problem #1 Given information Temperatures To Ti 32 F 68 F Thermal Resistance

More information

CME-TRUSS (Version 2.1) User's Manual

CME-TRUSS (Version 2.1) User's Manual CME-TRUSS (Version 2.1) User's Manual INTRODUCTION CME-TRUSS is an interactive program for structural analysis of two-dimensional trusses. The software is written in the Microsoft Visual Basic for Windows

More information

TRUS JOIST BEAMS, HEADERS, AND COLUMNS

TRUS JOIST BEAMS, HEADERS, AND COLUMNS FLOOR SOLUTIONS ROOF SOLUTIONS TRUS JOIST BEAMS, HEADERS, AND COLUMNS Featuring TimberStrand LSL, Parallam PSL, Microllam LVL, and Introducing the TimberStrand LSL Beam Uniform and Predictable Minimal

More information

THREE DIMENSIONAL ACES MODELS FOR BRIDGES

THREE DIMENSIONAL ACES MODELS FOR BRIDGES THREE DIMENSIONAL ACES MODELS FOR BRIDGES Noel Wenham, Design Engineer, Wyche Consulting Joe Wyche, Director, Wyche Consulting SYNOPSIS Plane grillage models are widely used for the design of bridges,

More information

Lindab We simplify construction. Table of contents

Lindab We simplify construction. Table of contents Table of contents 1 General information... 3 1.1 Platforms... 3 1.2 Licensing... 3 1.3 Database properties... 3 2 Display language... 4 3 Interface... 5 3.1 General Settings... 5 3.1.1 Country... 6 3.1.2

More information

CSiBridge 2015 (Version ) Release Notes

CSiBridge 2015 (Version ) Release Notes CSiBridge 2015 (Version 17.3.0) Release Notes Copyright Computers and Structures, Inc., 2015 Notice Date: 2015-07-02 This file lists all changes made to CSiBridge since the previous version. Most changes

More information

CE2302 STRUCTURAL ANALYSIS I Important Questions PART B

CE2302 STRUCTURAL ANALYSIS I Important Questions PART B CE2302 STRUCTURAL ANALYSIS I Important Questions PART B UNIT I 1. Determine the vertical and horizontal displacement of the joint B in a pin jointed frame shown in fig. 2. The cross sectional area of each

More information

LESM. Linear Elements Structure Model. Version 1.0 August Luiz Fernando Martha

LESM. Linear Elements Structure Model. Version 1.0 August Luiz Fernando Martha LESM Linear Elements Structure Model Version 1.0 August 2017 http://www.tecgraf.puc-rio.br/lesm by Luiz Fernando Martha (lfm@tecgraf.puc-rio.br) Rafael Lopez Rangel (rafaelrangel@tecgraf.puc-rio.br) Pontifical

More information

Tekla Structures Analysis Guide. Product version 21.0 March Tekla Corporation

Tekla Structures Analysis Guide. Product version 21.0 March Tekla Corporation Tekla Structures Analysis Guide Product version 21.0 March 2015 2015 Tekla Corporation Contents 1 Getting started with analysis... 7 1.1 What is an analysis model... 7 Analysis model objects...9 1.2 About

More information

ANALYSIS OF PLANE FRAME STRUCTURE WITH MATLAB AND SAP2000 PROGRAMS

ANALYSIS OF PLANE FRAME STRUCTURE WITH MATLAB AND SAP2000 PROGRAMS ANALYSIS OF PLANE FRAME STRUCTURE WITH MATLAB AND SAP2000 PROGRAMS Abdul Ahad FAIZAN Master Student, Dept. of Civil Engineering, Sakarya University, Sakarya, Turkey ---------------------------------------------------------------------***---------------------------------------------------------------------

More information

TSTOWER FOR SELF-SUPPORTING LATTICED TOWERS

TSTOWER FOR SELF-SUPPORTING LATTICED TOWERS TSTOWER FOR SELF-SUPPORTING LATTICED TOWERS STRUCTURAL ANALYSIS SOFTWARE FOR COMMUNICATION TOWERS USER S MANUAL BY JOHN WAHBA, PH.D., P.ENG., P.E. MATTHEW MALINOWSKI, P.ENG. WWW.TOWERSFT.COM TABLE OF CONTENTS

More information

General modeling guidelines

General modeling guidelines General modeling guidelines Some quotes from industry FEA experts: Finite element analysis is a very powerful tool with which to design products of superior quality. Like all tools, it can be used properly,

More information

SAFI Sample Projects. Design of a Steel Structure. SAFI Quality Software Inc. 3393, chemin Sainte-Foy Ste-Foy, Quebec, G1X 1S7 Canada

SAFI Sample Projects. Design of a Steel Structure. SAFI Quality Software Inc. 3393, chemin Sainte-Foy Ste-Foy, Quebec, G1X 1S7 Canada SAFI Sample Projects Design of a Steel Structure SAFI Quality Software Inc. 3393, chemin Sainte-Foy Ste-Foy, Quebec, G1X 1S7 Canada Contact: Rachik Elmaraghy, P.Eng., M.A.Sc. Tel.: 1-418-654-9454 1-800-810-9454

More information

Florida Building Code Online

Florida Building Code Online Florida Building Code Online http://www.floridabuilding.org/pr/pr_app_dtl.aspx?param=wgevxqwtdqsxyieb4opodd... Page 1 of 2 12/2/2010 BCIS Home Log In User Registration Hot Topics Submit Surcharge Stats

More information

Bridge Design using the STAAD.Pro/Beava AASHTO Code

Bridge Design using the STAAD.Pro/Beava AASHTO Code Bridge Design using the STAAD.Pro/Beava AASHTO Code By IEG Group, Bentley Systems Bentley Systems Inc. March 12, 2008 TABLE OF CONTENTS 1.0 Introduction.1 2.0 Creating the Bridge Geometry/Structural Analysis

More information

Advanced Application 1. Steel Structure

Advanced Application 1. Steel Structure Advanced Application 1 Steel Structure Steel Structure Summary Figure 1.1 Steel Building 1 Structural Plans & Section 1 2 3 4 36000 12000 12000 12000 E C4 SG1 SG1 SG1 C2 C2 C4 SG1A D C B A 38400 10800

More information

The Generate toolbar has convenient tools to create typical structural shapes.

The Generate toolbar has convenient tools to create typical structural shapes. Frame Analysis Using Multiframe 1. The software is on the computers in the College of Architecture in Programs under the Windows Start menu (see https://wikis.arch.tamu.edu/display/helpdesk/computer+accounts

More information

ANALYSIS OF BOX CULVERT - COST OPTIMIZATION FOR DIFFERENT ASPECT RATIOS OF CELL

ANALYSIS OF BOX CULVERT - COST OPTIMIZATION FOR DIFFERENT ASPECT RATIOS OF CELL ANALYSIS OF BOX CULVERT - COST OPTIMIZATION FOR DIFFERENT ASPECT RATIOS OF CELL M.G. Kalyanshetti 1, S.A. Gosavi 2 1 Assistant professor, Civil Engineering Department, Walchand Institute of Technology,

More information

Kully Reference Book

Kully Reference Book Kully Reference Book Serving the Greater Mid-West since 1946 Angles Channels Beams Rounds Sheets Squares Flats Rebar Wire Mesh Black & Galvanized Pipe Anchor Bolts Plastic, Copper, Black, Galvanized Pipe

More information

Simulation of AJWSP10033_FOLDED _ST_FR

Simulation of AJWSP10033_FOLDED _ST_FR Phone: 01922 453038 www.hyperon-simulation-and-cad-services.co.uk Simulation of AJWSP10033_FOLDED _ST_FR Date: 06 May 2017 Designer: Study name: AJWSP10033_FOLDED_STATIC Analysis type: Static Description

More information

Optimization of hanger arrangement of network arch bridges

Optimization of hanger arrangement of network arch bridges IABSE-JSCE Joint Conference on Advances in Bridge Engineering-II, August 8-10, 2010, Dhaka, Bangladesh. ISBN: 978-984-33-1893-0 Amin, Okui, Bhuiyan (eds.) www.iabse-bd.org Optimization of hanger arrangement

More information

UNIVERSITI MALAYSIA SARAWAK FACULTY OF ENGINEERING CIVIL ENGINEERING DEPARTMENT

UNIVERSITI MALAYSIA SARAWAK FACULTY OF ENGINEERING CIVIL ENGINEERING DEPARTMENT UNIVERSITI MALAYSIA SARAWAK FACULTY OF ENGINEERING CIVIL ENGINEERING DEPARTMENT KNS 1461 CIVIL ENGINEERING LABORATORY 2 LABORATORY MANUAL (Edited : December 2008) CIVIL ENGINEERING LABORATORY 2 KNS 1461

More information

General Information... 1 Introduction... 2 Getting started Starting a project Project management... 6

General Information... 1 Introduction... 2 Getting started Starting a project Project management... 6 Tutorial Tutorial Steel Hall AISC (AISC Steel 360-10) Hall Tutorial Frame Steel All information in this document is subject to modification without prior notice. No part or this manual may be reproduced,

More information

AASHTOWare BrD/BrR 6.8 Reinforced Concrete Structure Tutorial RC6 Two Span Reinforced Concrete Slab System Example

AASHTOWare BrD/BrR 6.8 Reinforced Concrete Structure Tutorial RC6 Two Span Reinforced Concrete Slab System Example AASHTOWare BrD/BrR 6.8 Reinforced Concrete Structure Tutorial RC6 Two Span Reinforced Concrete Slab System Example AASHTOWare Bridge Design and Rating Training 6" A A 30'-0" 30'-0" B #11's #11's 1'-6"

More information

General Applications

General Applications Chapter General Applications The general analysis modules can be used to calculate section properties, wind pressures on buildings and evaluate drainage systems of building roofs. General Applications

More information

Modelling Flat Spring Performance Using FEA

Modelling Flat Spring Performance Using FEA Modelling Flat Spring Performance Using FEA Blessing O Fatola, Patrick Keogh and Ben Hicks Department of Mechanical Engineering, University of Corresponding author bf223@bath.ac.uk Abstract. This paper

More information

CRUSHED STONE, 12" DEPTH CRUSHED STONE, 12" DEPTH (P) 920.845.1042 (F) 920.845.1048 Barrier Nettg Calculations Project Location: Prepared for: Madison, Wiscons Beacon Athletics - Middleton, WI REI Project

More information

STL1 - Simple Span Plate Girder Example

STL1 - Simple Span Plate Girder Example STL1 - Simple Span Plate Girder Example 1'-9" 47'-6" 44'-0" 1'-9" 10" including 1/2" int. wearing surface 4'-3" 3 spaces @ 13'-0" = 39'-0" 4'-3" 13'-0" 13'-0" 13'-0" 6 spaces @ 26'-10" 161'-0" Framing

More information

CE2351-STRUCTURAL ANALYSIS II

CE2351-STRUCTURAL ANALYSIS II CE2351-STRUCTURAL ANALYSIS II QUESTION BANK UNIT-I FLEXIBILITY METHOD PART-A 1. What are determinate structures? 2. What is meant by indeterminate structures? 3. What are the conditions of equilibrium?

More information

Tutorial AISC Steel Frame Building

Tutorial AISC Steel Frame Building Tutorial AISC 360-05 Steel Frame Building Tutorial Frame Steel All information in this document is subject to modification without prior notice. No part or this manual may be reproduced, stored in a database

More information

WP1 NUMERICAL BENCHMARK INVESTIGATION

WP1 NUMERICAL BENCHMARK INVESTIGATION WP1 NUMERICAL BENCHMARK INVESTIGATION 1 Table of contents 1 Introduction... 3 2 1 st example: beam under pure bending... 3 2.1 Definition of load application and boundary conditions... 4 2.2 Definition

More information

CE371 Structural Analysis II Lecture 5:

CE371 Structural Analysis II Lecture 5: CE371 Structural Analysis II Lecture 5: 15.1 15.4 15.1) Preliminary Remarks 15.2) Beam-Member Stiffness Matrix 15.3) Beam-Structure Stiffness Matrix 15.4) Application of the Stiffness Matrix. 15.1) Preliminary

More information

DEVELOPMENT OF THE THIN-WALL-2 PROGRAM FOR BUCKLING ANALYSIS OF THIN-WALLED SECTIONS UNDER GENERALISED LOADING

DEVELOPMENT OF THE THIN-WALL-2 PROGRAM FOR BUCKLING ANALYSIS OF THIN-WALLED SECTIONS UNDER GENERALISED LOADING Eighth International Conference on ADVANCES IN STEEL STRUCTURES Lisbon, Portugal, July 22-24, 2015 DEVELOPMENT OF THE THIN-WALL-2 PROGRAM FOR BUCKLING ANALYSIS OF THIN-WALLED SECTIONS UNDER GENERALISED

More information

WoodWorks Design Office User Guide U.S. Sizer Tutorial Instructions

WoodWorks Design Office User Guide U.S. Sizer Tutorial Instructions WoodWorks Design Office Sizer Shearwalls Connections Database Editor 2017 User Guide U.S. Sizer Tutorial Instructions For U.S. Design Office 11 Canadian Wood Council American Wood Council Developed by

More information

Q3 Thin-walled Cross Section. FRILO Software GmbH As of 01/03/2017 Version 2/2016

Q3 Thin-walled Cross Section. FRILO Software GmbH   As of 01/03/2017 Version 2/2016 Q3 Thin-walled Cross Section FRILO Software GmbH www.frilo.com info@frilo.com As of 01/03/2017 Version 2/2016 Q3 Q3 Thin-walled Cross Section Contents Application options 4 Basis of calculation 6 Definition

More information

SPECIFICATION AND GRADE YIELD EXT % TENSILE Y/T ELONG % (IN ) MIN: MAX: QT - QUENCH & TEMPERED SR - STRESS RELIEVED AR - AS ROLLED

SPECIFICATION AND GRADE YIELD EXT % TENSILE Y/T ELONG % (IN ) MIN: MAX: QT - QUENCH & TEMPERED SR - STRESS RELIEVED AR - AS ROLLED DATE: 08/8/4 UNITED STATES STEEL CORPORATION TUBULAR S TIME: 07:5:58 CERTIFIED REPORT SERIAL NO: L005857 (IN ACCORDANCE WITH ISO 0474/EN004/DIN50049 "type.") MILL ORDER/ITEM NO SHIPPERS NO. P.O. NUMBER

More information

Calculate Wind Pressure due to Hurricanes

Calculate Wind Pressure due to Hurricanes Calculate Wind Pressure due to Hurricanes ASCE 7-05 Method 2 Importance Factor ASCE 7-05 Sectoin 6.5.5 Residential building are Category I When V > 00 When V < 00 I =.0 Gust Effect Factor ASCE 7-05 Section

More information

Design of simple drapery systems to guide the rock falls along the slope

Design of simple drapery systems to guide the rock falls along the slope Design of simple drapery systems to guide the rock falls along the slope Simple drapery with the mesh opened at the bottom Simple drapery with the mesh fixed at the bottom Top cable? Top anchors? Mesh?

More information

Investigation of the behaviour of single span reinforced concrete historic bridges by using the finite element method

Investigation of the behaviour of single span reinforced concrete historic bridges by using the finite element method Structural Studies, Repairs and Maintenance of Heritage Architecture XI 279 Investigation of the behaviour of single span reinforced concrete historic bridges by using the finite element method S. B. Yuksel

More information

Inelastic Analysis of Seismic Loading of Precast Concrete Cladding Using Commercially Available Software

Inelastic Analysis of Seismic Loading of Precast Concrete Cladding Using Commercially Available Software San Jose State University SJSU ScholarWorks Master's Theses Master's Theses and Graduate Research Summer 2014 Inelastic Analysis of Seismic Loading of Precast Concrete Cladding Using Commercially Available

More information

(618) FAX (618)

(618) FAX (618) All STEEL PRODUCTS, Inc. Steel Pipe 1/8 through 120 O.D. Mechanical Squares & Rectangulars 1/2 thru 4 Square Equal Rectangulars Structural Squares & Rectangulars 1-1/2 thru 16 Square Equal Rectangulars

More information

SYLLABUS, MAJOR TOPICS & COMPUTERS

SYLLABUS, MAJOR TOPICS & COMPUTERS Introduction REINFORCED CONCRETE Reinforced Concrete Design A Fundamental Approach - Fifth Edition Fifth Edition SYLLABUS, MAJOR TOPICS & COMPUTERS A. J. Clark School of Engineering Department of Civil

More information

Connection Solutions

Connection Solutions Connection Solutions Connection Solutions for Cold formed Steel Construction Complies with; AS/NZS 4600:2005 AISI S100:2007 AS/NZ 1397 ASTM A653 www.framecad.com FRAMECAD Connectors are designed for speed,

More information

GT STRUDL. Version 29.1 Release Guide Volume 1 of 1. June 2007

GT STRUDL. Version 29.1 Release Guide Volume 1 of 1. June 2007 GT STRUDL Version 29.1 Release Guide Volume 1 of 1 June 2007 Computer-Aided Structural Engineering Center School of Civil & Environmental Engineering Georgia Institute of Technology Atlanta, Georgia 30332-0355

More information

GBTUL 1.0. Buckling and Vibration Analysis of Thin-Walled Members USER MANUAL. Rui Bebiano Nuno Silvestre Dinar Camotim

GBTUL 1.0. Buckling and Vibration Analysis of Thin-Walled Members USER MANUAL. Rui Bebiano Nuno Silvestre Dinar Camotim GBTUL 1.0 Buckling and Vibration Analysis of Thin-Walled Members USER MANUAL Rui Bebiano Nuno Silvestre Dinar Camotim Department of Civil Engineering and Architecture, DECivil/IST Technical University

More information

GT STRUDL. GT STRUDL Release Guide Version Volume 1 of 1

GT STRUDL. GT STRUDL Release Guide Version Volume 1 of 1 GT STRUDL GT STRUDL Release Guide Version 28.1 Volume 1 of 1 January 2006 Computer-Aided Structural Engineering Center School of Civil & Environmental Engineering Georgia Institute of Technology Atlanta,

More information

Tutorial 4 Arch Bridge

Tutorial 4 Arch Bridge Tutorial 4 Arch Bridge Civil TUTORIAL 4. ARCH BRIDGE Summary 1 Analysis Model and Load Cases / 2 File Opening and Preferences Setting 5 Enter Material and Section Properties 6 Structural Modeling Using

More information

Tutorial 1: Welded Frame - Problem Description

Tutorial 1: Welded Frame - Problem Description Tutorial 1: Welded Frame - Problem Description Introduction In this first tutorial, we will analyse a simple frame: firstly as a welded frame, and secondly as a pin jointed truss. In each case, we will

More information

C. Topkaya, J. A. Yura, E. B. Williamson, and K. H. Frank Research Report

C. Topkaya, J. A. Yura, E. B. Williamson, and K. H. Frank Research Report Technical Report Documentation Page 1. Report No. 2. Government Accession No. 3. Recipient s Catalog No. FHWA/TX-03/1898-3 4. Title and Subtitle 5. Report Date UTrAp: Finite-Element-Based Software for

More information

DIFFERENT TECHNIQUES FOR THE MODELING OF POST-TENSIONED CONCRETE BOX-GIRDER BRIDGES

DIFFERENT TECHNIQUES FOR THE MODELING OF POST-TENSIONED CONCRETE BOX-GIRDER BRIDGES DIFFERENT TECHNIQUES FOR THE MODELING OF POST-TENSIONED CONCRETE BOX-GIRDER BRIDGES Deepak Rayamajhi Naveed Anwar Jimmy Chandra Graduate Student Associate Director Graduate Student Structural Engineering

More information

Advanced 3-D Tutorial

Advanced 3-D Tutorial Advanced 3-D Tutorial Introduction To demonstrate some of the features of VisualAnalysis we have put together this advanced tutorial for you to use. This tutorial assumes that you have a basic knowledge

More information

Teaching Structural Behavior with a Physics Engine. Kirk Martini 1. VA 22904; PH ;

Teaching Structural Behavior with a Physics Engine. Kirk Martini 1. VA 22904; PH ; Teaching Structural Behavior with a Physics Engine Kirk Martini 1 1 University of Virginia, Department of Architecture, PO Box 400122, Charlottesville VA 22904; PH 434-924-6445; email: martini@virginia.edu

More information

Pro MECHANICA STRUCTURE WILDFIRE 4. ELEMENTS AND APPLICATIONS Part I. Yves Gagnon, M.A.Sc. Finite Element Analyst & Structural Consultant SDC

Pro MECHANICA STRUCTURE WILDFIRE 4. ELEMENTS AND APPLICATIONS Part I. Yves Gagnon, M.A.Sc. Finite Element Analyst & Structural Consultant SDC Pro MECHANICA STRUCTURE WILDFIRE 4 ELEMENTS AND APPLICATIONS Part I Yves Gagnon, M.A.Sc. Finite Element Analyst & Structural Consultant SDC PUBLICATIONS Schroff Development Corporation www.schroff.com

More information

Analysis of Composite Aerospace Structures Finite Elements Professor Kelly

Analysis of Composite Aerospace Structures Finite Elements Professor Kelly Analysis of Composite Aerospace Structures Finite Elements Professor Kelly John Middendorf #3049731 Assignment #3 I hereby certify that this is my own and original work. Signed, John Middendorf Analysis

More information