Advanced Application 1. Steel Structure
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1 Advanced Application 1 Steel Structure
2
3 Steel Structure Summary Figure 1.1 Steel Building 1
4 Structural Plans & Section E C4 SG1 SG1 SG1 C2 C2 C4 SG1A D C B A SG5 SG3 SG5 C3 C3 C4 SG1 SG1 SG6 SG4 SG3 SG4 C1 SG2 C1 SB1 SG2 SG2 SG2 C1A SG2 C1A SG4 SG3 SG4 C1 C1 SG1 SG1 SG1 SG1 SG1 C2A C2A SG1 SG1 SG4 SG3A SG4 SG4 SG4 SG4 C6 C6 C6 C3A C3A C4A SG2 SG1 C5 C5 SG4 SG3A SG4 SG1 SG C6 C6 C7 SG1 SG1 C5 C5 C5A C6 C6 C7 SG1 SG4 SG1 SG1 SG1 SG1 SG4 SG4 SG3A SG5 SG5 SG3 C6 SG1 C SG B' C' D' E' A' Element Name Section ID DB Section Size SG1 221 AISC W24x76 SG2 222 AISC W18x55 SG3 223 AISC W18x55 SG4 224 AISC W12x136 SG5 225 AISC W24x103 SG6 226 AISC W18x86 SB1 231 AISC W12x26 SG1A 241 AISC W12x53 SG3A 243 AISC W24x76 Figure 1.2 Structural Plan of the lower part (2~4F) 2
5 E C4 SG1 SG1 SG1 C2 C2 C4 D C B SG5 SG3 SG5 SCG1 C3 C3 C4 SG1 SG1 SG4 SG3 SG4 C1 SG2 SG2 C1A C1 SB1 SG2 SG2 SG2 C1A SG4 SG3 SG4 C1 SG1 SG1 C1 SG5 SG3 SG5 C3A C3A SG1 SG1 SG1 SB2 C2A SB2 C2A SB2 C4A SCG1 SCG1 SCG1 Element Name Section ID DB Section Size SG1 521 AISC W24x76 SG2 522 AISC W21x62 SG3 523 AISC W14x48 SG4 524 AISC W27x129 SG5 525 AISC W24x103 SB1 531 AISC W12x26 SB2 532 AISC W8x31 SCG1 571 AISC W14x34 Figure 1.3 Structural Plan of the upper part (5~Roof) 3
6 Roof 15F 14F 13F 12F = F 10F 9F F 7F 6F =22.8 5F 4F F 2F 6.0 1F 단위 Unit: : m Figure 1.4 The cross section (Section 2) 4
7 Applied Codes Applied Load / UBC(1997) Steel Design Code / AISC(14th)-LRFD10 SRC Design Code / SSRC79 Used Materials Beam, Brace: A36 Column: A Concrete Grade C4000 Applied Loads Gravity loads unit: kn/m 2 Use Shop Office Roof Floor , Roof Dead Load Live Load Wind loads Basic Wind Speed: 80 mph Exposure Category: C Importance Factor: 1.0 Pressure Coefficient: 1.3 5
8 Seismic Load Seismic Zone Factor: Z = 1 (0.075) Importance Factor: 1.0 Soil Coefficient: Sc Height of the building: Hn = 64 m Width of the building: Bx = m, By = m Response Modification Coefficient Rx: 4.2 (Steel with steel OMRF) Ry: 4.2 (Steel with steel OMRF) Unit Load Cases Load Case Number Name Applied loads Static Load Cases Dynamic Load Cases 1 Self Self weight 2 DL Dead Load 3 LL Live Load 4 WX 5 WY RX RY Wind Load (X-direction in the global coordinates) Wind Load (Y-direction in the global coordinates) Response Spectrum Seismic Load (X-direction in the global coordinates) Response Spectrum Seismic Load (Y-direction in the global coordinates) 6
9 Structural Modeling Initial Window & Unit System Setting File > New Project File > Save (Steel) Tools > Setting > Unit System or Status Bar Length > m ; Force > N Point Grid (off), Point Grid Snap (off), Line Grid Snap (off) 7
10 Figure 1.5 Initial Window Setting 8
11 Input Material Property & Section Data Property Number Name Type Property Type 1 Girder Steel A36 2 Steel Column Steel A53 3 SRC Column SRC A53 + Grade Brace Steel A36 Table 1.1 Used material properties Properties > Material > Name > Girder ; Standard > ASTM(S) ; Material Properties Type > Steel DB > A36 Name > Steel Column ; Type > Steel Standard > ASTM(S) ; DB > A Name > SRC Column ; Type > SRC Steel Standard > ASTM(S) ; DB > A Concrete Standard > ASTM(RC) ; DB > Grade C4000 Name > Brace ; Type > Steel Standard > ASTM(S) ; DB > A36. 9
12 Figure 1.6 Input material properties Figure 1.7 Input the section data of the lower part girders (refer Figure 1.2 for section sizes) 10
13 Input the 2nd floor Elements Hidden (on), Node Number (on), Element Number (on) Structure > Wizard > Base Structure > Frame Input tab X Coord. / Distance > 12 ; Repeat > 3 Z Coord./ Distance > 10.8 ; Repeat > 2 Z Coord./ Distance > 6 ; Repeat > 1 Z Coord./ Distance > 10.8 ; Repeat > 1 Edit tab Beta Angle > 90 Deg. Material > 1 ; Section > 221 Click. Insert tab Insert Point > 0, 0, 6 Rotations / Alpha > -90. Click. Zoom Fit Figure 1.8 Create the 2nd floor elements using Frame Wizard 11
14 Node/Element > Elements > Material Name> 1:Girder Section Name > 226:SG6 Create Element Nodal Connectivity > 2, 5 Material Name> 1:Girder Section Name > 222:SG2 Nodal Connectivity > Element 33 (Refer to Figure 1.9) Material Name> 1:Girder Section Name > 231:SB1 Nodal Connectivity > Element 36 (Refer to Figure 1.9) Figure 1.9 Modify the 2nd floor elements Top View Select Window (Node 1) Select Element 1, 16 Click Delete key 12
15 Display > Node > Node Number (off) Tree Menu > Works tab Select Single (8, 11, 34, 35, 37, 38) Display > Property > Property Name (on) Properties > Section > 222:SG2 (Drag & Drop) Similarly change properties of SG1 to SG3A, SG4 & SG5 by Drag & Drop (Refer to Figure 1.2) Drop Drag Figure 1.10 Change the section numbers using Drag & Drop 13
16 UCS & Line Grid Setting Node Number (on) Display > Property > Property Name (off) X-Y Coordinates Origin > 36, 10.8, 6 (Node 8) Angle > -30 Define Line Grid Grid Name > Skew Plane X-Grid Lines Line > 2@12. Y-Grid Lines Levels > -10.8, 2@10.8, 6, 10.8 Add/Modify Grid Lines Zoom Fit (on), Line Grid Snap (on) Figure 1.12 Define the grid lines 14
17 Figure 1.13 UCS & Line Grid setting Create Elements of the Skewed Part Node/Elements > Elements > Section Name > 221:SG1 Create Elements Nodal Connectivity > Node 4 & corner of Line Grid (Refer to of Figure 1.14) Create the Remainders (Refer to Figure 1.15) 15
18 Figure 1.14 Input SG1 of the 2nd floor of the skewed part Figure 1.15 Input the beam element of the 2nd floor of the skewed part 16
19 Select Single (unnecessary node & element; of Figure 1.15) Delete Display GCS (on), Line Grid (off), Line Grid Snap (off) Figure 1.16 Delete the unnecessary node and element 17
20 Input the Beam End Release Conditions Display > Property > Property Name (on) Select Single (SB1-element 36) Boundary > Release/Offset > Beam End Release (Refer to of Figure 1.17). Figure 1.17 Input the Beam End Release condition 18
21 The following column section data have been inputted in the file Steel(import).mgb C1 C1A Unit Story Section Section Steel RC Number Number Steel RC 6 14~ W W ~ W W ~ W W ~7 103 W W ~4 102 W W ~2 101 W W C2 C2A Unit Story Section Section Steel RC Number Number Steel RC 6 14~ W W ~ W W ~ W W ~7 203 W W ~4 202 W W ~2 201 W W Table 1.2 Column Section Data (1) 19
22 C3 C3A Unit Story Section Number Steel RC Section Number Steel RC 6 14~ W W ~ W W ~ W W ~7 303 W W ~4 302 W W ~2 301 W W C4 C4A Unit Story Section Number Steel RC Section Number Steel RC 6 14~ W W ~ W W ~ W W ~7 403 W W ~4 402 W W ~2 401 W W C5 C5A Unit Story Section Number DB Steel Section Number DB Steel AISC W AISC W ~2 501 AISC W AISC W C6 C7 Unit Story Section Number DB Steel Section Number DB Steel AISC W AISC W ~2 601 AISC W AISC W Table 1.2 Column Section Data (2) 20
23 Typical method for inputting SRC sections: Properties > Section > Section Properties Add> SRC tab Section ID > 101 ; Name > C1 Shape > Rect-IBeam Concrete Data HC > 0.7 ; BC > 0.7 Steel Data / DB > AISC Steel Name > W Material > Concrete Material>DB>ASTM(RC) Concrete Material / Name > Grade C4000 Steel Material>DB>ASTM(S) Steel Material / Name > A Replace steel (on) ; Shear Deformation (on) Figure 1.18 Input SRC Sections 21
24 Properties > Section > Section Properties > ( of Figure 1.19) Application folder > Steel(import).mgb Import the column section data > (Refer to Figure 1.20) Figure 1.19 Section data before Import 22
25 Figure 1.20 Input the section data using import function 23
26 Input Columns Redraw Node Number (on) Display > Property > Property Name (off) Iso View, Rotate Dynamic Zoom Fit (Refer to Figure 1.21) Select All Unselect Window (Node 23, 24) Node/Element > Elements > Extrude Elements Extrude Type > Node Line Element Reverse I-J (on) ; Material > 3 : SRC Column ; Generation Type > Translate ; Element Type > Beam Section > 101 : C1 Translate > Equal Distance Beta angle > 0 ; Number of Times > 1 dx, dy, dz > 0, 0, -6 Display > Element > Local Direction (on) Display > Element > Local Direction (off) 24
27 Figure 1.21 Create the columns of the 1st floor 25
28 Select Recent Entities (Columns) Node/Element > Elements > Change Element Parameters Parameter Type > Element Local Axis Mode > Assign > Beta Angle > 90 Select Previous Unselect Polygon (Columns with Beta Angle = 90 ) Beta Angle > 60 Select Single (Refer to of Figure 1.22) Assign > Beta Angle > -30 Figure 1.22 Unselect Polygon 26
29 Status bar > Filter > z (Columns) Select All Unselect Polygon (Columns) (Refer to Figure 1.23) Tree Menu > Works tab Properties > Material > 2 : Steel Column (Drag & Drop) Select All, Active, Node Number (off) Display > Property > Property Name (on) Select Single (Elements 83, 84) (Refer to Figure 1.24) Properties > Section > 151 : C1A (Drag & Drop) Modify the others in the same way (Refer to Figure 1.2) Active All 27
30 Drag Drop Figure 1.23 Modify beta angles and material properties Drop Drag Figure 1.24 Modify the column number using Drag & Drop 28
31 Input the Diagonal Elements X-direction Y-direction Story Section Section Section size Number Number Section size W W W W Table 1.3 Section list of the diagonal elements Figure 1.25 Input the Brace section data 29
32 Shrink (off) Zoom Window (core part) Node Number (on), Node/Element > Elements > Element Number (on) Create Elements Element Type > Truss Material Name > 4 : Brace Section Name > 1001 : BR1 Nodal Connectivity > X-directional Braces (Refer to Figure 1.26) Section No. > 2001:BR2 Nodal Connectivity > Y-directional Braces (Refer to Figure 1.26) Figure 1.26 Input the Braces 30
33 Building Generation Auto Fitting (on) Node Number (off), Elements Number (off) Status bar > Filter > none Select All Structure > Building > Control Data > Building Generation Building Generation > Number of Copies > 2 Distance(Global Z) > 5 ; Operations > Building Generation > Number of Copies > 6 Distance(Global Z) > 3.8 ; Operations > Building Generation > Number of Copies > 6 Distance(Global Z) > 4.2 ; Operations > Building Generation Table> Insert the increment of the section numbers (Refer to Figure 1.27) Copy Element Attributes (on) > Boundaries > Beam Release (on) Figure 1.27 Building Generation Table 31
34 Select Plane XY Plane > Z Position > 64 Active Display > Boundary > Beam End release Symbol (on) Display > Boundary > Beam End release Symbol (off) Figure 1.28 Building Generation 32
35 Modify the upper part of the model Element Name Section Number Section Size SG1 521 W SG2 522 W SG3 523 W SG4 524 W SG5 525 W SB1 531 W SB2 532 W 8 31 SCG1 571 W Table 1.4 Sections of the upper part beams/girders Active All, Top View Select Polygon + Ctrl key in Keyboard (Top View of Figure 1.29) Front View Unselect Window (Front View of Figure 1.29) Iso View Delete Key in Keyboard (Selected Nodes & Elements) 33
36 Top view Front view Figure 1.29 Select the non-existent elements 34
37 Select-Identity Element Select Type > Section List > 243, Right View Unselect Window (Refer to Figure 1.31) Iso View Tree Menu > Works tab Properties>Section > 523:SG3 (Drag & Drop) Select-Identity Element Select Type > Section List > 224 : SG4, Top View Unselect Window (Refer to Figure 1.31) Tree Menu/ Works tab Properties > Section > 525:SG5 (Drag & Drop) Iso View 35
38 Right View Iso View Figure 1.30 Modify the model using Unselect Window and Works Tree 36
39 Figure 1.31 Modify the model using Unselect Window Drop Drag Figure 1.32 Modify the upper part of the model 37
40 Input Story Data Structure > Building > Control Data > Story Figure 1.33 Story Data 38
41 Input the Cantilever Beams Structure > UCS/Plan > Named Plane Plane Name > B Plane Type > X-Z Plane Y Position > 10.8 Select All Active Identity > Named Plane > B, Display > Node > Story Name (on) Display > Boundary > Beam End release Symbol (on) Figure 1.34 Activate the Named Plane 39
42 Node/Element > Elements > Extrude Elements Extrude Type > Node Line Element > Reverse I-J (on) Element Type > Beam ; Material > 1:Girder Section > 571:SCG1 Equal Distance > dx, dy, dz > 0, -1.2, 0 Number of Times > 1 Select Polygon (Nodes over the 5th Floor) Node/Element > Elements > Create Elements Element Type > General beam/tapered beam Material > 1:Girder ; Section No. > 532:SB2 Zoom Window (the grid of the 5th Floor) Nodal Connectivity > 637 Zoom Fit Zoom Window (the grid of the 5th Floor) Zoom Window (off) Nodal Connectivity > 637, 640 Figure 1.35 Input the Cantilever Beam 40
43 Zoom Fit Select Recent Entities Boundary > Release/Offset > Beam End Release Select Previous Node/Element > Elements > Translate Elements Translation > Unequal Distance Axis > Z Distances > 5@3.8, 6@4.2 Copy Node Attributes (on) Copy Element Attributes (on) Figure 1.36 Copy the outer Cantilever Beam 41
44 Input the Boundary Conditions Active All Display > Node > Story Name (on) Select Plane XY Plane > Z Position > 0 Boundary > Supports > Define Supports D-All (on) ; R-All (on) Figure 1.37 Input the Support Condition of the structure 42
45 Input Loads Load Cases Setting Load > Static Load Cases Input as Figure 1.38 Figure 1.38 Static unit load case setting Input Self-weight Refer to other Tutorials. 43
46 Input the Floor Loads Load > Static Loads > Initial Forces/Misc. > Assign Floor Loads Load Type > Define Floor Load Type (Refer to Figure 1.39) Refer to Applied Loads on page 5. Figure 1.39 Define Floor Load Type 44
47 Active Identity Story > 2F +Below (on), Node Number (on) Hidden (off) Angle View Horizontal > 50 ; Vertical > 60 Load > Static Loads > Initial Forces/Misc. > Assign Floor Loads Load Type > Shop Distribution Type > One Way ; Load Angle (A1) > 0 No. of Sub Beams > 3 ; Sub Beam Angle (A2) > 90 Unit Self Weight > 883 N/m ; Load Direction > Global Z ; Copy Floor Load (on) Projection > Yes Axis > Z ; Distances > 5 Nodes Defining Loading Area > 4,12, 9, 5, 2, 4 Figure 1.40 Input the Floor Loads 45
48 Nodes Defining Loading Area > 17, 13, 16, 20, 17 Nodes Defining Loading Area > 25, 28, 27, 8, 4, 25 Nodes Defining Loading Area > 30, 32, 31, 29, 30 Figure 1.41 Input the Floor Loads of the skewed part 46
49 Load Angle(A1) > 90 Sub-Beam Angle(A2) > 0 Nodes Defining Loading Area > 12, 27, 8, 12 Nodes Defining Loading Area > 20, 31, 29, 16, 20 Display > Load > Floor Load Name (on) Figure 1.42 Confirm the inputted floor loads by Floor Load Name 47
50 No. of Sub Beams > 1 Nodes Defining Loading Area > 16, 29, 27, 12, 16 Nodes Defining Loading Area > 13, 14,10, 9, 13 Nodes Defining Loading Area > 15, 16, 12, 11, 15 Nodes Defining Loading Area > 29, 30, 28, 27, 29 No. of Sub Beams > 0 Nodes Defining Loading Area > 22, 21, 23, 24, 22 Active All Figure 1.43 Confirm the inputted floor loads by Floor Load Name 48
51 Active Identity Story > 4F +Below (on), Display > Load > Floor Load Name (off) Load Type > Office Distribution Type > One Way Load Angle (A1) > 90 No. of Sub Beams > 3 Sub-Beam Angle (A2) > 0 Unit Self Weight > 883 N/m Copy Floor Load (on) ; Axis > z Distances > 6@3.8, 5@4.2 Nodes Defining Loading Area > 124, 127, 123, 120, 124 Input the others in the same way (Refer to Figure 1.44) Node Number (off) Active All, Front View Tree Menu > Works tab 49
52 Figure 1.44 Loading Plan of the upper part over the 4th floor Figure 1.45 Confirm the inputted floor loads on the upper Office 50
53 Active Identity Story > 4F ; +Below (on), Angle View Horizontal > 50 ; Vertical > 60 Zoom Fit Load Type > roof ; Description > 4F roof Copy Floor Load (off) Nodes Defining Loading Area > Roof Loads * Notice: Load Angle, Sub-Beam Angle, Number of Sub Beams Figure 1.46 Input the 4th floor loads 51
54 Figure 1.47 Confirm the inputted loads by Works Tree 52
55 Active Identity Story > 5F ; +Below (on), Load Type > Office Distribution Type > One Way No. of Sub Beams > 0 Description > Delete Copy Floor Load (on) Z Axis Distances > 5@3.8, 5@4.2 Nodes Defining Loading Area > Cantilever *Consider Load Angle (A1) Active Identity Story > 15F ; +Below (on) Figure 1.48 Input the Floor Loads of the upper part cantilever 53
56 Active Identity Story > Roof ; +Below (on), Load Type > roof No. of Sub Beams > 3 Copy Floor Load (off) Nodes Defining Loading Area > Roof Floor Cantilever portion: No. of Sub Beams > 0 Active All Assign Floor Loads > Floor Load Table > (Refer to Figure 1.50) Figure 1.49 Input the floor loads of the roof 54
57 Figure 1.50 Floor Load Table 55
58 Input the Wind Loads Structure > Building > Control Data > Story Wind tab ( of Figure 1.51) Figure 1.51 Story Data 56
59 Load > Lateral Loads > Wind Loads Load Case Name > WX Wind Load Code > UBC(1997) Projected Area Method > (on) ; Exposure Category > C ; Basic Wind Speed > 80 Importance Factor > 1 ; Pressure Coefficient > 1.3 Scale Factor in Global Y > 1 ; Scale Factor in Global Y > 0 Story Shear (GL) > N Load Case Name > WY Wind Load Code > UBC(1997) Projected Area Method > (on) ; Exposure Category > C ; Basic Wind Speed > 80 Importance Factor > 1 ; Pressure Coefficient > 1.3 Scale Factor in Global X > 0 ; Scale Factor in Global Y > 1 Story Shear (GL) > N Figure 1.52 Dialog box to input the wind load 57
60 Figure 1.53 Wind Load Profile 58
61 Figure 1.54 Wind loads calculation 59
62 Input the Response Spectrum Analysis Conditions Structure > Type > Structure Type Converting Type of Model weight to Masses > Convert to X, Y Gravity Acceleration > Align Top of Beam Section to Floor(X-Y Plane) for Panel Zone Effect/Display (on) Load > Structure Loads/Masses > Nodal Masses > Loads to Masses Mass Direction > X, Y Load Type for Converting > all (on) Load Case > DL ; Scale Factor > 1 Query > Story Mass Table Figure 1.55 Create the mass data automatically 60
63 Figure 1.56 Story Mass Table 61
64 Load > Seismic > Response Spectrum Data > Response Spectrum Load Case Number of Frequencies > 15 Figure 1.57 Eigenvalue analysis conditions setting Modal Combination Control > Modal Combination Type > SRSS Design Spectrum > UBC(1997) Seismic Coefficients Calculation Option > Automatic (on) Soil Profile Type (S) > Sc Seismic Zone Factor (Z) > 1 (0.075) Seismic Coefficient (Ca) > 0.09 Seismic Coefficient (Cv) > 0.13 Max. Period > 10 (sec) Scale Factor (IE/R) > (Refer to Figure 1.59) 62
65 Figure 1.58 Assign the method of the mode combination Figure 1.59 Dialog box to create the Design Spectrum automatically 63
66 Load > Seismic > Response Spectrum Data > Response Spectrum Load Case Load Case Name > RX Direction > X-Y Excitation Angle > 0 Scale Factor > 1 Period Modification Factor > 1 Function Name > UBC1997 (on) Operations > Load Case Name > RY Excitation Angle > 90 Operations > Figure 1.60 Input the response spectrum load cases 64
67 Perform the Structural Analysis/Window Setting Analysis > Perform Analysis Figure 1.61 Toolbar setting to confirm the results 65
68 Confirm the Analysis Results Examine Reactions Tools > Setting > Unit System Force > kn Active Identity Story > 2F ; +Below (on), Results > Results > Reactions > Reaction Forces/Moments Load Case/Combinations > ST : DL Components > FZ Type of Display > Values (on), Legend (on) Values > Decimal Points > 2 Results > Tables > Result Tables > Reaction Load Combination > Self(ST) (on), DL(ST) (on), LL(ST) (on) 66
69 Figure 1.62 Confirm the reactions in the gravity direction Figure Reaction Table
70 Examine the Eigenvalue Analysis Results Results > Tables > Result Tables > Vibration Mode Shape Active Dialog > Node No. Governing Direction Participation Masses (%) Period(sec) 1 ROTN-Z TRAN-X TRAN-Y Figure 1.64 Confirm the Eigenvalue analysis results 68
71 Model View tab Iso View, Active All, Initial View Results > Vibration Mode Shapes Load Cases (Mode Numbers) > Mode 1 Components > Md-XYZ (on) Type of Display > Mode Shape > Mode Shape Scale Factor > 3.0 Animate (on) > Animation Mode > Repeat Full Cycle Record Stop Close Figure 1.65 Vibration Mode Shapes 69
72 Steel Member Design Applied Design Code: AISC(14th)-LRFD10 Create the Load Combinations All Windows except Model View > Results > Combinations > Load Combination Steel Design tab Design Code > AISC(14th)-LRFD10 Scale Up Factor > 2.719, RX Scale Up Factor > 2.504, RY Figure 1.66 Input the Design Code & the Scale Up Factor 70
73 Figure 1.67 Create the load combinations Input the Design Parameters Design > General Design Parameter > Definition of Frame X-Direction Frame > Braced I Non-sway Y-Direction Frame > Braced I Non-sway Design Type > 3-D (on) Figure 1.68 Definition of Frame 71
74 Initial View Select Identity-Element Select Type > Section List > 221 : SG1 List > 226 : SG6 List > 521 : 5SG1 Design > General Design Parameter > Unbraced Length (L, Lb) Add > Replace > (on) Laterally Unbraced Length Lb > 4 Input the remainders ; Refer to Table 1.5 Figure 1.69 Input lateral unbraced lengths 72
75 Section Number Laterally Unbraced Length (m) , 226, , 225, 524, , 223, 243, 522, Table 1.5 Laterally Unbraced Length of the girders Design > Design > Steel Design > Design Code Design Code > AISC(14th)-LRFD10 All Beams/Girders are Laterally Braced (on) Figure 1.70 Select the design code 73
76 Steel Code Check Redraw Design > Design > Steel Design > Steel Code Check Result View Option > NG (Refer to Figure 1.71) Property No. > 224 Select (SEL) W (Refer to Figure 1.73) Select (SEL) > Property No. > 224 (Refer to Figure 1.72) Figure 1.71 Automatic Design Result Dialog box 74
77 Figure 1.72 Summary of Design Results 75
78 Figure 1.73 Change Steel Properties Dialog box Design > Section > Section for Design 1001 > W ; 1002 > W ; 2001 > W Select Identity-Element > Select Type > Section 224(on), 1001(on), 1002(on), 2001(on) Design > Design > Steel > Steel Code Check Figure 1.74 Code Checking Result Dialog box after modifying the sections 76
79 Unselect All Design > Design > Steel > Steel Code Check Result View Option > All Select (SEL) > 221 Ratio Limit > From > 0 ; To > 0.75 Figure 1.75 Modify section numbers using the design results 77
80 Model View tab The right side of Select Identity-Element (Refer to of Figure 1.76) [Ctrl]+[C] in Keyboard (Copy Command) Figure 1.76 Select elements to modify the sections 78
81 Re-analyze/Re-design reflecting the Design Results Code Checking Result Dialog > Select (SEL) > 224(on), 1001(on), 1002(on), 2001(on) (Refer to Figure 1.77) Analysis / design results will be deleted. Continue? The right side of Select Identity-Element (Refer to of Figure 1.76) [Ctrl]+[V] in Keyboard (Paste Command) Model > Elements > Change Element Parameters Parameter Type > Section ID Assign No. > 522 Analysis > Perform Analysis OR Re-analysis (Refer to Figure 1.78) Figure 1.77 Update Changed Properties Dialog 79
82 Figure 1.78 Dialog box after updating the selected sections Figure 1.79 Modify sections using the Change Element Parameter 80
83 Select Identity-Element Select Type > Section List > 224:SG4, 522:SG2, 1001:BR1, 1002:BR1, 2001:BR2 Design > Steel Code Check (Refer to Figure 1.80) Select (SEL) > 224 (Refer to Figure 1.81) Figure 1.80 Confirm the results of the re-design 81
84 Figure 1.81 Stress ratio graph of 2 4F SG1 (after modifying sections) 82
85 SRC Column Design Applied Design Code: SSRC79 Create the Load Combinations Unselect All Result > Combination > Load Combination SRC Design tab Option > Add (on) Design Code > SSRC79 Scale Up Factor > 2.719, RX Scale Up Factor > 2.504, RY Figure 1.82 Select the SRC Design Code 83
86 Input the Design Parameters Design > Design > SRC Design > Design Code Design Code > SSRC79 Tools > Setting > Unit System Length > cm Design > Design > SRC Design > Modify SRC Column Section Data SEL > Section ID > 151 ~ 156 Reinforcing Main Bar > Auto Calculate Rebar Space (on) Rebar > 12 - #8 Number of Rows > 4 Figure 1.83 Modify SRC Column Section Data 84
87 SRC Code Check Design > Design > SRC Design > SRC Code Check > Column Checking Figure 1.84 SRC Code Checking Result Dialog 85
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