Successful Applications of CFD within the Aircraft Certification Process TLG Aerospace. Unrestricted Siemens AG 2018

Size: px
Start display at page:

Download "Successful Applications of CFD within the Aircraft Certification Process TLG Aerospace. Unrestricted Siemens AG 2018"

Transcription

1 Successful Applications of CFD within the Aircraft Certification Process TLG Aerospace Unrestricted Siemens AG 2018

2 About TLG Aerospace TLG is an engineering services company providing design, analysis, test, and certification expertise to help bring client products to market. TLG uses Siemens STAR-CCM+ and NASTRAN to develop full-vehicle certification models for loads, flutter, and handling qualities. FAA Designated Engineering Representatives (DER) on staff: Loads, Flutter, Flight Analyst, Stress. Core expertise in aerodynamics, structures and design. High-end analysis capabilities include fluid-structure interaction, dynamic free-body interactions, non-linear structural dynamics. Robert Lind, Director of Engineering, FAA Flutter DER Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 2

3 Analysis in the Certification process The FAA requires certification by test, or by analysis that is validated by test. Method of Compliance varies for different regulations. CFD plays an increasing role in expediting the certification process and lowering costs. Reducing the number of flight test conditions Enabling safer flight testing by predictive analysis of potential hazards Enabling test to lower load levels with analytical extrapolation to higher load levels Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 3

4 Full Vehicle Models FAA loads and flutter analyses require full-vehicle models coupling aerodynamics, mass properties, structural dynamics, and flight controls. Proper modelling of fluid-structure interaction is a critical requirement for certification. Industry standard techniques for rapid and accurate FSI over the entire flight envelope, steady and unsteady. The integrated full-vehicle model is ultimately validated by flight test and must be shown to be accurate or conservative. Aeroelastic Model Aerodynamics CFD, Low Order Methods, Wind Tunnel, Handbook Validation by pressure, strain measurements in flight test Mass Properties CAD, Weights Bookkeeping Validation by weighing Full Vehicle Model Structures Finite Element Analysis, Handbook Validation by GVT, static load in ground test Flight Controls Flight Control Laws Validation by integrated sim and flight test Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 4

5 How is CFD Consumed? CFD results are mapped to a reduced order aerodynamic model within an aeroelastic process: Doublet Lattice Method (DLM) in NASTRAN is typical. Linear and non-linear aerodynamic treatments available. Manipulated to ensure accurate or conservative predictions from the full vehicle model. Reduced order model will produce steady and unsteady flexible and rotary aerodynamics. A local linearization from CFD is used to scale the reduced order model. Final aeroelastic model will reproduce full-vehicle integrated and distributed aerodynamics from CFD when run in rigid mode. Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 5

6 How is CFD Consumed? Calibrated aeroelastic model will yield a converged, trimmed, aeroelastic solution in seconds. Wing span-load scaling for a transport Airplane Each curve represents a unique wing station. Flying surfaces scaled to match sectional properties on a spanwise basis. Pressures can be projected to reduced order model, or mapped directly. Extracting Pressure Load on a Windscreen and Fixed Leading Edge Segment Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 6

7 CFD or and Wind Tunnel Wind Tunnel testing remains a critical tool for aerodynamic configuration development and handling qualities assessment. Wind tunnel best for incipient separation regimes (e.g. high-alpha and Sideslip handling qualities). CFD good for moderate-alpha and sideslip and detail flow-field investigation. A hybrid CFD and Wind Tunnel strategy will often yield the best results. Both data sources can be assimilated into the full vehicle model. CFD is increasingly used in a Virtual Wind Tunnel mode to develop large aerodynamic databases for certification. Where accurate or conservative linearization can be performed. Enabled by innovative licensing strategies and breakthroughs in elastic cloud computing. TLG uses STAR-CCM+ to generate databases with thousands of cases. Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 7

8 Modern CFD Productivity Notional Notional Assumptions: Accuracy of each approach assumed suitable for the application. Model Costs: LSWT $165k, HSWT: $315k, CFD (Legacy/Now): $15k / $15k Usage Rate (per Hour): LSWT: $600, HSWT: $4500, CFD (Legacy/ Now): $250 / $100 Engineers per Hour: LSWT: x2, HSWT: x3, CFD (Legacy/ Now): x1 / x1 Productivity: LSWT: 800 cond/day, HSWT: 600 cond/day, CFD (Legacy/ Now): 20 / 80 cases/day Disclaimer, calculations may differ for your specific application. Large databases can be run in STAR-CCM+ today at a fraction of the cost and schedule of legacy methods and wind tunnel testing. Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 8

9 100% Spot Instances Shared File System Mounted to Head (NFS to Compute Nodes) AES 256 Encryption Elastic Computing with P.O.D. Licensing Virtual HPC Environment Cluster ABC ABC01 Head Node ABC02 Compute ABC03 Compute ABC04 Compute ABC05 Compute Large RANK Security Group Gateway Secure Elastic Cloud Computing Multiple Clusters Cold Storage Simple Storage Secure Tunnel Power-On-Demand licensing and elastic cloud computing eliminates the serial execution bottleneck. Unlimited throughput in theory. No technical limitation to running vast numbers of CFD cases simultaneously. Practical limitation is human resources. Scalable to large models. Elastic computing allows most models to be run in < 1-hour, regardless of model size. Secure Terminal On-premise Sync Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 9

10 Other Applications of CFD in Certification Pressure loading on secondary structures, fairings, antennas and radomes. Non-impact assessment to original type compliance due to modifications. Flap effectiveness in Star-CCM+ validated against OEM test data Internal flows of inlets/outlets/ducts. Air-data system location. Reduced Vertical Separation Minimums (RVSM) performance. Particle trajectory analysis for safe separation of ice and non-damage tolerant structures. Static source error analysis in Star-CCM+ validation in flight test Ice accretion analysis. Cavity Resonance Analysis in Star-CCM+ Non-impact Assessment Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 10

11 Summary CFD is increasingly used in the certification process as a supplement or replacement to wind tunnel testing. CFD informs the full vehicle model that is ultimately validated by test and shown to be accurate or conservative. Power-on-Demand licensing and elastic cloud computing enables large numbers of CFD simulations to be performed in a short time and for low cost. Siemens STAR-CCM+ is routinely used for aircraft certification at TLG Aerospace and has contributed to receipt of numerous FAA approved Supplemental Type Certificates Successful Applications of CFD within the Aircraft Certification Process TLGAerospace.com 11

Air Force Materiel Command

Air Force Materiel Command Air Force Materiel Command Developing, Fielding, and Sustaining America s Aerospace Force High-Fidelity Physics- Based Modeling in Support of Test & Evaluation Dr. Ed Kraft AEDC/CZ NDIA M&S Conference

More information

COURSE: Aeroelasticity

COURSE: Aeroelasticity SESSION WEEK COURSE: Aeroelasticity DEGREE: Aerospace Engineering YEAR: 4th TERM: 1st La asignatura tiene 29 sesiones que se distribuyen a lo largo de 14 semanas. Los laboratorios pueden situarse en cualquiera

More information

MSC/NASTRAN FLUTTER ANALYSES OF T-TAILS INCLUDING HORIZONTAL STABILIZER STATIC LIFT EFFECTS AND T-TAIL TRANSONIC DIP

MSC/NASTRAN FLUTTER ANALYSES OF T-TAILS INCLUDING HORIZONTAL STABILIZER STATIC LIFT EFFECTS AND T-TAIL TRANSONIC DIP MSC/NASTRAN FLUTTER ANALYSES OF T-TAILS INCLUDING HORIZONTAL STABILIZER STATIC LIFT EFFECTS AND T-TAIL TRANSONIC DIP by Emil Suciu* Gulfstream Aerospace Corporation Savannah, Georgia U.S.A. Presented at

More information

MSC Software Aeroelastic Tools. Mike Coleman and Fausto Gill di Vincenzo

MSC Software Aeroelastic Tools. Mike Coleman and Fausto Gill di Vincenzo MSC Software Aeroelastic Tools Mike Coleman and Fausto Gill di Vincenzo MSC Software Confidential 2 MSC Software Confidential 3 MSC Software Confidential 4 MSC Software Confidential 5 MSC Flightloads An

More information

Accurate and Efficient Turbomachinery Simulation. Chad Custer, PhD Turbomachinery Technical Specialist

Accurate and Efficient Turbomachinery Simulation. Chad Custer, PhD Turbomachinery Technical Specialist Accurate and Efficient Turbomachinery Simulation Chad Custer, PhD Turbomachinery Technical Specialist Outline Turbomachinery simulation advantages Axial fan optimization Description of design objectives

More information

OzenCloud Case Studies

OzenCloud Case Studies OzenCloud Case Studies Case Studies, April 20, 2015 ANSYS in the Cloud Case Studies: Aerodynamics & fluttering study on an aircraft wing using fluid structure interaction 1 Powered by UberCloud http://www.theubercloud.com

More information

THE EFFECTS OF THE PLANFORM SHAPE ON DRAG POLAR CURVES OF WINGS: FLUID-STRUCTURE INTERACTION ANALYSES RESULTS

THE EFFECTS OF THE PLANFORM SHAPE ON DRAG POLAR CURVES OF WINGS: FLUID-STRUCTURE INTERACTION ANALYSES RESULTS March 18-20, 2013 THE EFFECTS OF THE PLANFORM SHAPE ON DRAG POLAR CURVES OF WINGS: FLUID-STRUCTURE INTERACTION ANALYSES RESULTS Authors: M.R. Chiarelli, M. Ciabattari, M. Cagnoni, G. Lombardi Speaker:

More information

Towards a Lower Helicopter Noise Interference in Human Life

Towards a Lower Helicopter Noise Interference in Human Life Towards a Lower Helicopter Noise Interference in Human Life Fausto Cenedese Acoustics and Vibration Department AGUSTA, Via G. Agusta 520, 21017 Cascina Costa (VA), Italy Noise Regulation Workshop September

More information

The Use of Computational Fluid Dynamics In the Aerospace Industry Past Present - Future

The Use of Computational Fluid Dynamics In the Aerospace Industry Past Present - Future The Use of Computational Fluid Dynamics In the Aerospace Industry Past Present - Future Douglas N. Ball Aerospace Consultant 1 The Early Days Not much CFD in these old birds! Great airplanes none the less.

More information

Missile External Aerodynamics Using Star-CCM+ Star European Conference 03/22-23/2011

Missile External Aerodynamics Using Star-CCM+ Star European Conference 03/22-23/2011 Missile External Aerodynamics Using Star-CCM+ Star European Conference 03/22-23/2011 StarCCM_StarEurope_2011 4/6/11 1 Overview 2 Role of CFD in Aerodynamic Analyses Classical aerodynamics / Semi-Empirical

More information

FLUTTER ANALYSIS OF F-16 AIRCRAFT UTILIZING TEST MODAL DATA

FLUTTER ANALYSIS OF F-16 AIRCRAFT UTILIZING TEST MODAL DATA 25 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES FLUTTER ANALYSIS OF F-16 AIRCRAFT UTILIZING TEST MODAL DATA Kwan-Hwa Byun*, Seung-Moon Jun** *Agency for Defense Development (ADD), **ADD Keywords:

More information

Detached Eddy Simulation Analysis of a Transonic Rocket Booster for Steady & Unsteady Buffet Loads

Detached Eddy Simulation Analysis of a Transonic Rocket Booster for Steady & Unsteady Buffet Loads Detached Eddy Simulation Analysis of a Transonic Rocket Booster for Steady & Unsteady Buffet Loads Matt Knapp Chief Aerodynamicist TLG Aerospace, LLC Presentation Overview Introduction to TLG Aerospace

More information

An efficient method for predicting zero-lift or boundary-layer drag including aeroelastic effects for the design environment

An efficient method for predicting zero-lift or boundary-layer drag including aeroelastic effects for the design environment The Aeronautical Journal November 2015 Volume 119 No 1221 1451 An efficient method for predicting zero-lift or boundary-layer drag including aeroelastic effects for the design environment J. A. Camberos

More information

Aeroelasticity in MSC.Nastran

Aeroelasticity in MSC.Nastran Aeroelasticity in MSC.Nastran Hybrid Static Aeroelasticity new capabilities - CFD data management Presented By: Fausto Gill Di Vincenzo 04-06-2012 Hybrid Static Aeroelastic Solution with CFD data MSC.Nastran

More information

The Role of Finite Element Analysis in Light Aircraft Design and Certification

The Role of Finite Element Analysis in Light Aircraft Design and Certification The Role of Finite Element Analysis in Light Aircraft Design and Certification Nigel Bamber Wey Valley Aeronautics Ltd www.weyvalleyaero.co.uk Engineering Consultancy Civil and Military Aerospace and Motorsport

More information

INTEGRATION OF MSC.FLIGHTLOADS AND DYNAMICS AT LOCKHEED MARTIN AERONAUTICS COMPANY * Dan Egle Lockheed Martin Aeronautics Company Fort Worth, TX

INTEGRATION OF MSC.FLIGHTLOADS AND DYNAMICS AT LOCKHEED MARTIN AERONAUTICS COMPANY * Dan Egle Lockheed Martin Aeronautics Company Fort Worth, TX INTEGRATION OF MSC.FLIGHTLOADS AND DYNAMICS AT LOCKHEED MARTIN AERONAUTICS COMPANY * Dan Egle Lockheed Martin Aeronautics Company Fort Worth, TX John Ausman MSC.Software Corporation Santa Ana, CA Abstract

More information

Digital-X. Towards Virtual Aircraft Design and Testing based on High-Fidelity Methods - Recent Developments at DLR -

Digital-X. Towards Virtual Aircraft Design and Testing based on High-Fidelity Methods - Recent Developments at DLR - Digital-X Towards Virtual Aircraft Design and Testing based on High-Fidelity Methods - Recent Developments at DLR - O. Brodersen, C.-C. Rossow, N. Kroll DLR Institute of Aerodynamics and Flow Technology

More information

CAD-BASED WORKFLOWS. VSP Workshop 2017

CAD-BASED WORKFLOWS. VSP Workshop 2017 CAD-BASED WORKFLOWS VSP Workshop 2017 RESEARCH IN FLIGHT COMPANY Established 2012 Primary functions are the development, marketing and support of FlightStream and the development of aerodynamic solutions

More information

Impact of Computational Aerodynamics on Aircraft Design

Impact of Computational Aerodynamics on Aircraft Design Impact of Computational Aerodynamics on Aircraft Design Outline Aircraft Design Process Aerodynamic Design Process Wind Tunnels &Computational Aero. Impact on Aircraft Design Process Revealing details

More information

TAU mesh deformation. Thomas Gerhold

TAU mesh deformation. Thomas Gerhold TAU mesh deformation Thomas Gerhold The parallel mesh deformation of the DLR TAU-Code Introduction Mesh deformation method & Parallelization Results & Applications Conclusion & Outlook Introduction CFD

More information

Streamlining Aircraft Icing Simulations. D. Snyder, M. Elmore

Streamlining Aircraft Icing Simulations. D. Snyder, M. Elmore Streamlining Aircraft Icing Simulations D. Snyder, M. Elmore Industry Analysis Needs / Trends Fidelity Aircraft Ice Protection Systems-Level Modeling Optimization Background Ice accretion can critically

More information

Symmetric Maneuver Loads Module Development & Integration within an Aircraft Tracking Environment

Symmetric Maneuver Loads Module Development & Integration within an Aircraft Tracking Environment Symmetric Maneuver Loads Module Development & Integration within an Aircraft Tracking Environment 14 April 2015 Phoenix Integration Workshop Marina del Rey, CA Ned Lindsley, AFRL/QVC Remaining Useful Life

More information

High-Lift Aerodynamics: STAR-CCM+ Applied to AIAA HiLiftWS1 D. Snyder

High-Lift Aerodynamics: STAR-CCM+ Applied to AIAA HiLiftWS1 D. Snyder High-Lift Aerodynamics: STAR-CCM+ Applied to AIAA HiLiftWS1 D. Snyder Aerospace Application Areas Aerodynamics Subsonic through Hypersonic Aeroacoustics Store release & weapons bay analysis High lift devices

More information

863. Development of a finite element model of the sailplane fuselage

863. Development of a finite element model of the sailplane fuselage 863. Development of a finite element model of the sailplane fuselage M. Andrikaitis 1, A. Fedaravičius 2 Kaunas University of Technology, Kęstučio 27, 44312 Kaunas, Lithuania E-mail: 1 marius.andrikaitis@gmail.com,

More information

Incompressible Potential Flow. Panel Methods (3)

Incompressible Potential Flow. Panel Methods (3) Incompressible Potential Flow Panel Methods (3) Outline Some Potential Theory Derivation of the Integral Equation for the Potential Classic Panel Method Program PANEL Subsonic Airfoil Aerodynamics Issues

More information

Offshore Platform Fluid Structure Interaction (FSI) Simulation

Offshore Platform Fluid Structure Interaction (FSI) Simulation Offshore Platform Fluid Structure Interaction (FSI) Simulation Ali Marzaban, CD-adapco Murthy Lakshmiraju, CD-adapco Nigel Richardson, CD-adapco Mike Henneke, CD-adapco Guangyu Wu, Chevron Pedro M. Vargas,

More information

TILTAERO. Tilt Rotor Interactional Aerodynamics. Antonio Saporiti. AgustaWestland Cascina Costa (Italy) TILT ROTOR INTERACTIONAL AERODYNAMICS

TILTAERO. Tilt Rotor Interactional Aerodynamics. Antonio Saporiti. AgustaWestland Cascina Costa (Italy) TILT ROTOR INTERACTIONAL AERODYNAMICS TILTAERO Tilt Rotor Interactional Aerodynamics Antonio Saporiti AgustaWestland Cascina Costa (Italy) TILTAERO 1 TILTAERO Framework Program Competitive and Sustainable Growth Purpose Investigation of aerodynamic

More information

SPC 307 Aerodynamics. Lecture 1. February 10, 2018

SPC 307 Aerodynamics. Lecture 1. February 10, 2018 SPC 307 Aerodynamics Lecture 1 February 10, 2018 Sep. 18, 2016 1 Course Materials drahmednagib.com 2 COURSE OUTLINE Introduction to Aerodynamics Review on the Fundamentals of Fluid Mechanics Euler and

More information

Status of Gradient-based Airframe MDO at DLR The VicToria Project

Status of Gradient-based Airframe MDO at DLR The VicToria Project DLR.de Chart 1 Status of Gradient-based Airframe MDO at DLR The VicToria Project M. Abu-Zurayk, C. Ilic, A. Merle, A. Stück, S. Keye, A. Rempke (Institute of Aerodynamics and Flow Technology) T. Klimmek,

More information

CFD++ APPLICATION ON WIND TUNNEL DATA ANALYSIS

CFD++ APPLICATION ON WIND TUNNEL DATA ANALYSIS CFD++ APPLICATION ON WIND TUNNEL DATA ANALYSIS Introduction Piaggio Aero Industries is actually studing a new mid size jet for civilian use. Many people and many disciplines are implicated but up to now

More information

Coupling STAR-CCM+ with Optimization Software IOSO by the example of axial 8-stages jet engine compressor.

Coupling STAR-CCM+ with Optimization Software IOSO by the example of axial 8-stages jet engine compressor. Coupling STAR-CCM+ with Optimization Software IOSO by the example of axial 8-stages jet engine compressor. Folomeev V., (Sarov Engineering Center) Iakunin A., (JSC Klimov) 1 Objectives To create the procedure

More information

COURSE: Advanced Aeroelasticity

COURSE: Advanced Aeroelasticity SESSION WEEK COURSE: Advanced Aeroelasticity MASTER: Aerospace Engineering YEAR: 1st TERM: 2nd La asignatura tiene 28 sesiones que se distribuyen a lo largo de 14 semanas. Los laboratorios pueden situarse

More information

Your Home for Advanced Aerodynamic/ Aeroelastic/Aeroservoelastic/Computer Aided Engineering Software Products and Services

Your Home for Advanced Aerodynamic/ Aeroelastic/Aeroservoelastic/Computer Aided Engineering Software Products and Services Your Home for Advanced Aerodynamic/ Aeroelastic/Aeroservoelastic/Computer Aided Engineering Software Products and Services About ZONA ZONA Technology, Inc. (ZONA) is a privately held company that was founded

More information

HPC Considerations for Scalable Multidiscipline CAE Applications on Conventional Linux Platforms. Author: Correspondence: ABSTRACT:

HPC Considerations for Scalable Multidiscipline CAE Applications on Conventional Linux Platforms. Author: Correspondence: ABSTRACT: HPC Considerations for Scalable Multidiscipline CAE Applications on Conventional Linux Platforms Author: Stan Posey Panasas, Inc. Correspondence: Stan Posey Panasas, Inc. Phone +510 608 4383 Email sposey@panasas.com

More information

AERODYNAMIC MODELING USING FLIGHT MECHANICAL SIMULATIONS, FLIGHT TEST AND OPTIMIZATION

AERODYNAMIC MODELING USING FLIGHT MECHANICAL SIMULATIONS, FLIGHT TEST AND OPTIMIZATION 25 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AERODYNAMIC MODELING USING FLIGHT MECHANICAL SIMULATIONS, FLIGHT TEST AND OPTIMIZATION Per Weinerfelt*, Roger Larsson* Saab Aerosystems Flight

More information

Validation of an Unstructured Overset Mesh Method for CFD Analysis of Store Separation D. Snyder presented by R. Fitzsimmons

Validation of an Unstructured Overset Mesh Method for CFD Analysis of Store Separation D. Snyder presented by R. Fitzsimmons Validation of an Unstructured Overset Mesh Method for CFD Analysis of Store Separation D. Snyder presented by R. Fitzsimmons Stores Separation Introduction Flight Test Expensive, high-risk, sometimes catastrophic

More information

TAU User Meeting, Göttingen,

TAU User Meeting, Göttingen, TAU User Meeting, Göttingen, 22.9.2005 Fluid-Structure-Coupling Using the TAU Code: Developments and Applications at the DLR Institute of Aeroelasticity Wolf Krüger DLR Institute of Aeroelasticity Fluid-Structure-Coupling

More information

An advanced RBF Morph application: coupled CFD-CSM Aeroelastic Analysis of a Full Aircraft Model and Comparison to Experimental Data

An advanced RBF Morph application: coupled CFD-CSM Aeroelastic Analysis of a Full Aircraft Model and Comparison to Experimental Data An advanced RBF Morph application: coupled CFD-CSM Aeroelastic Analysis of a Full Aircraft Model and Comparison to Experimental Data Dr. Marco Evangelos Biancolini Tor Vergata University, Rome, Italy Dr.

More information

Why Supercomputing Partnerships Matter for CFD Simulations

Why Supercomputing Partnerships Matter for CFD Simulations Why Supercomputing Partnerships Matter for CFD Simulations Wim Slagter, PhD Director, HPC & Cloud Alliances ANSYS, Inc. 1 2017 ANSYS, Inc. May 9, 2017 ANSYS is Fluids FOCUSED This is all we do. Leading

More information

UNSTEADY RANS BASED IMPULSE RESPONSE STUDIES OF AGARD WING FOR AEROELASTIC AND FLUTTER ANALYSIS

UNSTEADY RANS BASED IMPULSE RESPONSE STUDIES OF AGARD WING FOR AEROELASTIC AND FLUTTER ANALYSIS Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2) November 68, 2, Bangalore, India UNSTEADY RANS BASED IMPULSE RESPONSE STUDIES OF AGARD WING FOR AEROELASTIC AND FLUTTER ANALYSIS

More information

computational Fluid Dynamics - Prof. V. Esfahanian

computational Fluid Dynamics - Prof. V. Esfahanian Three boards categories: Experimental Theoretical Computational Crucial to know all three: Each has their advantages and disadvantages. Require validation and verification. School of Mechanical Engineering

More information

ANSYS Fluid Structure Interaction for Thermal Management and Aeroelasticity

ANSYS Fluid Structure Interaction for Thermal Management and Aeroelasticity ANSYS Fluid Structure Interaction for Thermal Management and Aeroelasticity Phil Stopford Duxford Air Museum 11th May 2011 2011 2010 ANSYS, Inc. All rights reserved. 1 ANSYS, Inc. Proprietary Fluid Structure

More information

Advanced Computation in the design and development of aircraft engines. Serge Eury SNECMA

Advanced Computation in the design and development of aircraft engines. Serge Eury SNECMA Advanced Computation in the design and development of aircraft engines 1 Serge Eury SNECMA Advanced Computation in the design and development of aircraft engines Introduction Some examples Conclusions

More information

Simcenter Motion 3D. Mechatronics - Improve Design Dynamics Performance: Combine 3D Multi-Body Simulation with 1D Actuation & Controls Simulation

Simcenter Motion 3D. Mechatronics - Improve Design Dynamics Performance: Combine 3D Multi-Body Simulation with 1D Actuation & Controls Simulation Simcenter Motion 3D Mechatronics - Improve Design Dynamics Performance: Combine 3D Multi-Body Simulation with 1D Actuation & Controls Simulation Iurie TERNA Email: iurie.terna@siemens.com Tuesday 16:00-17:00

More information

Numerical Investigation of Transonic Shock Oscillations on Stationary Aerofoils

Numerical Investigation of Transonic Shock Oscillations on Stationary Aerofoils Numerical Investigation of Transonic Shock Oscillations on Stationary Aerofoils A. Soda, T. Knopp, K. Weinman German Aerospace Center DLR, Göttingen/Germany Symposium on Hybrid RANS-LES Methods Stockholm/Sweden,

More information

CFD Analysis of conceptual Aircraft body

CFD Analysis of conceptual Aircraft body CFD Analysis of conceptual Aircraft body Manikantissar 1, Dr.Ankur geete 2 1 M. Tech scholar in Mechanical Engineering, SD Bansal college of technology, Indore, M.P, India 2 Associate professor in Mechanical

More information

Advances in Turbomachinery Simulation Fred Mendonça and material prepared by Chad Custer, Turbomachinery Technology Specialist

Advances in Turbomachinery Simulation Fred Mendonça and material prepared by Chad Custer, Turbomachinery Technology Specialist Advances in Turbomachinery Simulation Fred Mendonça and material prepared by Chad Custer, Turbomachinery Technology Specialist Usage From Across the Industry Outline Key Application Objectives Conjugate

More information

SOLIDWORKS SIMULATION

SOLIDWORKS SIMULATION SOLIDWORKS SIMULATION Innovation is about taking chances, not taking risks Scootchi by Curventa Designworks LTD What if? is the question that fuels innovation. SolidWorks Simulation software takes the

More information

Fluid-Structure Interaction Over an Aircraft Wing

Fluid-Structure Interaction Over an Aircraft Wing International Journal of Engineering Research and Development e-issn: 2278-067X, p-issn: 2278-800X, www.ijerd.com Volume 13, Issue 4 (April 2017), PP.27-31 Fluid-Structure Interaction Over an Aircraft

More information

Team 194: Aerodynamic Study of Airflow around an Airfoil in the EGI Cloud

Team 194: Aerodynamic Study of Airflow around an Airfoil in the EGI Cloud Team 194: Aerodynamic Study of Airflow around an Airfoil in the EGI Cloud CFD Support s OpenFOAM and UberCloud Containers enable efficient, effective, and easy access and use of MEET THE TEAM End-User/CFD

More information

UNSTEADY TAU AND ROM FOR FLUTTER COMPUTATIONS OF TRANSPORT AIRCRAFT. Reik Thormann, Ralph Voß. Folie 1

UNSTEADY TAU AND ROM FOR FLUTTER COMPUTATIONS OF TRANSPORT AIRCRAFT. Reik Thormann, Ralph Voß. Folie 1 UNSTEADY TAU AND ROM FOR FLUTTER COMPUTATIONS OF TRANSPORT AIRCRAFT Reik Thormann, Ralph Voß Folie 1 Standardfoliensatz >01.03.2007 Outline Motivation Synthetic Mode Correction (SMC) Linearized CFD Method

More information

Complete and robust mechanical simulation solution. imaginit.com/simulation-mechanical

Complete and robust mechanical simulation solution. imaginit.com/simulation-mechanical Complete and robust mechanical simulation solution A mechanical simulation solution for finite element analysis powered by the Autodesk Nastran solver Accurately predict product behavior, optimize and

More information

imaginit.com/simulation Complete and robust mechanical simulation solution

imaginit.com/simulation Complete and robust mechanical simulation solution imaginit.com/simulation Complete and robust mechanical simulation solution A mechanical simulation solution for finite imaginit.com/simulation element analysis powered by the Autodesk Nastran solver Accurately

More information

Introduction to Computational Fluid Dynamics Mech 122 D. Fabris, K. Lynch, D. Rich

Introduction to Computational Fluid Dynamics Mech 122 D. Fabris, K. Lynch, D. Rich Introduction to Computational Fluid Dynamics Mech 122 D. Fabris, K. Lynch, D. Rich 1 Computational Fluid dynamics Computational fluid dynamics (CFD) is the analysis of systems involving fluid flow, heat

More information

Can Wing Tip Vortices Be Accurately Simulated? Ryan Termath, Science and Teacher Researcher (STAR) Program, CAL POLY SAN LUIS OBISPO

Can Wing Tip Vortices Be Accurately Simulated? Ryan Termath, Science and Teacher Researcher (STAR) Program, CAL POLY SAN LUIS OBISPO AFFTC-PA-11316 Can Wing Tip Vortices Be Accurately Simulated? A F F T C m Ryan Termath, Science and Teacher Researcher (STAR) Program, CAL POLY SAN LUIS OBISPO Jason Lechniak, and Keerti Bhamidipati AIR

More information

1 Introduction. 2 Simulation and experimental works. Acta Polytechnica Vol. 44 No. 2/2004

1 Introduction. 2 Simulation and experimental works. Acta Polytechnica Vol. 44 No. 2/2004 Acta Polytechnica Vol. 44 No. 2/24 Computational Fluid Dynamic Simulation (CFD) and Experimental Study on Wing-external Store Aerodynamic Interference of a Subsonic Fighter Aircraft Tholudin Mat Lazim,

More information

Recent & Upcoming Features in STAR-CCM+ for Aerospace Applications Deryl Snyder, Ph.D.

Recent & Upcoming Features in STAR-CCM+ for Aerospace Applications Deryl Snyder, Ph.D. Recent & Upcoming Features in STAR-CCM+ for Aerospace Applications Deryl Snyder, Ph.D. Outline Introduction Aerospace Applications Summary New Capabilities for Aerospace Continuity Convergence Accelerator

More information

NUMERICAL EVALUATION OF THE CONTRIBUTION OF THE STICK MODEL-INDUCED ELASTIC STREAMWISE CAMBER DEFORMATION TO THE FLUTTER SPEED OF A SWEPT WING

NUMERICAL EVALUATION OF THE CONTRIBUTION OF THE STICK MODEL-INDUCED ELASTIC STREAMWISE CAMBER DEFORMATION TO THE FLUTTER SPEED OF A SWEPT WING NUMERICAL EVALUATION OF THE CONTRIBUTION OF THE STICK MODEL-INDUCED ELASTIC STREAMWISE CAMBER DEFORMATION TO THE FLUTTER SPEED OF A SWEPT WING Paper No. 2004-23, Presented at the MSC.Software Virtual Product

More information

Unrestricted Siemens AG 2016 Realize innovation.

Unrestricted Siemens AG 2016 Realize innovation. Automation and Standardization of CFD Workflows Dr. Wolfram Kühnel, MAHLE Behr GmbH & Co. KG Unrestricted Siemens AG 2016 Realize innovation. Outline The company Globalization Standardization Automation

More information

AERODYNAMIC DESIGN OF FLYING WING WITH EMPHASIS ON HIGH WING LOADING

AERODYNAMIC DESIGN OF FLYING WING WITH EMPHASIS ON HIGH WING LOADING AERODYNAMIC DESIGN OF FLYING WING WITH EMPHASIS ON HIGH WING LOADING M. Figat Warsaw University of Technology Keywords: Aerodynamic design, CFD Abstract This paper presents an aerodynamic design process

More information

INVESTIGATION ON STRUCTURAL ASPECTS OF UNMANNED COMBAT AIR VEHICLE FOR AEROELASTIC ANALYSIS P N Vinay *, P V Srihari *, A Mahadesh Kumar

INVESTIGATION ON STRUCTURAL ASPECTS OF UNMANNED COMBAT AIR VEHICLE FOR AEROELASTIC ANALYSIS P N Vinay *, P V Srihari *, A Mahadesh Kumar Research Article INVESTIGATION ON STRUCTURAL ASPECTS OF UNMANNED COMBAT AIR VEHICLE FOR AEROELASTIC ANALYSIS P N Vinay *, P V Srihari *, A Mahadesh Kumar Address for Correspondence * Dept. of Mechanical

More information

Fluid-Structure Interaction in STAR-CCM+ Alan Mueller CD-adapco

Fluid-Structure Interaction in STAR-CCM+ Alan Mueller CD-adapco Fluid-Structure Interaction in STAR-CCM+ Alan Mueller CD-adapco What is FSI? Air Interaction with a Flexible Structure What is FSI? Water/Air Interaction with a Structure Courtesy CFD Marine Courtesy Germanischer

More information

Loads Analysis and Structural Optimization - A Parameterized and Integrated Process

Loads Analysis and Structural Optimization - A Parameterized and Integrated Process DLR.de Chart 1 Loads Analysis and Structural Optimization - A Parameterized and Integrated Process Thomas Klimmek (AE), Thiemo Kier (SR), Andreas Schuster (FA), Tobias Bach (FA), and Dieter Kohlgrüber

More information

EXPERIMENTAL VALIDATION OF STAR-CCM+ FOR LIQUID CONTAINER SLOSH DYNAMICS

EXPERIMENTAL VALIDATION OF STAR-CCM+ FOR LIQUID CONTAINER SLOSH DYNAMICS EXPERIMENTAL VALIDATION OF STAR-CCM+ FOR LIQUID CONTAINER SLOSH DYNAMICS Brandon Marsell a.i. solutions, Launch Services Program, Kennedy Space Center, FL 1 Agenda Introduction Problem Background Experiment

More information

FLUID COMPUTING. ARC FORUM, India Ricky Watts Director of Industrial Solutions, Wind River IN A SOFTWARE-DEFINED WORLD

FLUID COMPUTING. ARC FORUM, India Ricky Watts Director of Industrial Solutions, Wind River IN A SOFTWARE-DEFINED WORLD FLUID COMPUTING IN A SOFTWARE-DEFINED WORLD ARC FORUM, India Ricky Watts Director of Industrial Solutions, Wind River Chemical Sector Commercial Building Sector Communications Sector Critical Manufacturing

More information

CFD Methods for Aerodynamic Design

CFD Methods for Aerodynamic Design CFD Methods for Aerodynamic Design Afandi Darlington Optimal Aerodynamics Ltd Why CFD? Datasheet methods are still very relevant today (ESDU, USAF DATCOM) Validated estimates of lift, drag, moments, stability

More information

Development Of Computational Tools For Analysis And Evaluation Of Autonomous Parafoil Systems

Development Of Computational Tools For Analysis And Evaluation Of Autonomous Parafoil Systems Development Of Computational Tools For Analysis And Evaluation Of Autonomous Parafoil Systems Esteban Gonzalez Garcia, Carlos G. Sacco, Aula CIMNE IUA Enrique Ortega, Roberto Flores, CIMNE Barcelona 2do

More information

Cyber Security Technologies

Cyber Security Technologies 1 / Cyber Security Technologies International Seminar on Cyber Security: An Action to Establish the National Cyber Security Center Lisbon, 12 th September 2013 23 / Key highlights - Thales Group Thales

More information

Fluid structure interaction analysis: vortex shedding induced vibrations

Fluid structure interaction analysis: vortex shedding induced vibrations Fluid structure interaction analysis: vortex shedding induced vibrations N. Di Domenico, M. E. * University of Rome «Tor Vergata», Department of Enterprise Engineering «Mario Lucertini» A. Wade, T. Berg,

More information

University of Texas VSP Structural Analysis Module Update - Demonstration

University of Texas VSP Structural Analysis Module Update - Demonstration University of Texas VSP Structural Analysis Module Update - Demonstration http://vspsam.ae.utexas.edu/ VSP Workshop, San Luis Obispo, CA Hersh Amin Armand J. Chaput Department of Aerospace Engineering

More information

Advancing Computerized Wind-Loading Tests to the Next Level Hi-Res CFD for Wind Loading of Tall Buildings

Advancing Computerized Wind-Loading Tests to the Next Level Hi-Res CFD for Wind Loading of Tall Buildings Advancing Computerized Wind-Loading Tests to the Next Level Hi-Res CFD for Wind Loading of Tall Buildings Nick Wirth, Founder, Wirth Research Rob Rowsell, Engineering Manager, Wirth Research Wirth Research

More information

Computational Fluid Dynamics PRODUCT SHEET

Computational Fluid Dynamics PRODUCT SHEET TM 2014 Computational Fluid Dynamics PRODUCT SHEET 1 Breaking Limitations The Challenge of Traditional CFD In the traditional mesh-based approach, the reliability highly depends on the quality of the mesh,

More information

Cloud Security Gaps. Cloud-Native Security.

Cloud Security Gaps. Cloud-Native Security. Cloud Security Gaps Cloud-Native Security www.aporeto.com Why Network Segmentation is Failing Your Cloud Application Security How to Achieve Effective Application Segmentation By now it s obvious to security-minded

More information

Recent Approaches of CAD / CAE Product Development. Tools, Innovations, Collaborative Engineering.

Recent Approaches of CAD / CAE Product Development. Tools, Innovations, Collaborative Engineering. Recent Approaches of CAD / CAE Product Development. Tools, Innovations, Collaborative Engineering. Author: Dr.-Ing. Peter Binde Abstract: In this paper, the latest approaches in the field of CAD-CAE product

More information

OpenVSP: Parametric Geometry for Conceptual Aircraft Design. Rob McDonald, Ph.D. Associate Professor, Cal Poly

OpenVSP: Parametric Geometry for Conceptual Aircraft Design. Rob McDonald, Ph.D. Associate Professor, Cal Poly OpenVSP: Parametric Geometry for Conceptual Aircraft Design Rob McDonald, Ph.D. Associate Professor, Cal Poly 1 Vehicle Sketch Pad (VSP) Rapid parametric geometry for design NASA developed & trusted tool

More information

Discover better designs, faster.

Discover better designs, faster. Discover better designs, faster. Design of next-generation rotorcraft systems Benefits: Reduced testing Lower development cost Faster-to-market rotorcrafts Fully optimized designs and safer vehicles Improved

More information

Numerical Simulations of Fluid-Structure Interaction Problems using MpCCI

Numerical Simulations of Fluid-Structure Interaction Problems using MpCCI Numerical Simulations of Fluid-Structure Interaction Problems using MpCCI François Thirifay and Philippe Geuzaine CENAERO, Avenue Jean Mermoz 30, B-6041 Gosselies, Belgium Abstract. This paper reports

More information

Enabling SMEs to benefit from HPC based OpenFOAM simulation services Carmen Cotelo, CESGA

Enabling SMEs to benefit from HPC based OpenFOAM simulation services Carmen Cotelo, CESGA Enabling SMEs to benefit from HPC based OpenFOAM simulation services Carmen Cotelo, CESGA fortissimo@cesga.es 2nd Iberian meeting of OpenFOAM technology users. Santiago de Compostela 28-29 May 2018 1 Fortissimo

More information

THE APPLICATION OF AN ATMOSPHERIC BOUNDARY LAYER TO EVALUATE TRUCK AERODYNAMICS IN CFD

THE APPLICATION OF AN ATMOSPHERIC BOUNDARY LAYER TO EVALUATE TRUCK AERODYNAMICS IN CFD THE APPLICATION OF AN ATMOSPHERIC BOUNDARY LAYER TO EVALUATE TRUCK AERODYNAMICS IN CFD A SOLUTION FOR A REAL-WORLD ENGINEERING PROBLEM Ir. Niek van Dijk DAF Trucks N.V. CONTENTS Scope & Background Theory:

More information

39th AIAA Aerospace Sciences Meeting and Exhibit January 8 11, 2001/Reno, NV

39th AIAA Aerospace Sciences Meeting and Exhibit January 8 11, 2001/Reno, NV AIAA 1 717 Static Aero-elastic Computation with a Coupled CFD and CSD Method J. Cai, F. Liu Department of Mechanical and Aerospace Engineering University of California, Irvine, CA 92697-3975 H.M. Tsai,

More information

Coupling OpenFOAM and MBDyn with precice coupling tool

Coupling OpenFOAM and MBDyn with precice coupling tool Coupling OpenFOAM and MBDyn with precice coupling tool Mikko Folkersma Faculty of Aerospace Engineering Section of Wind Energy Delft University of Technology Delft, The Netherlands Outline 1. Introduction

More information

5504 Thermocouple Analog Input Module

5504 Thermocouple Analog Input Module 550 Thermocouple Analog Input Installation, Operation and Maintenance Setup Manual 5/9/0 Safety Information The information provided in this documentation contains general descriptions and/or technical

More information

Keisuke Sawada. Department of Aerospace Engineering Tohoku University

Keisuke Sawada. Department of Aerospace Engineering Tohoku University March 29th, 213 : Next Generation Aircraft Workshop at Washington University Numerical Study of Wing Deformation Effect in Wind-Tunnel Testing Keisuke Sawada Department of Aerospace Engineering Tohoku

More information

Modern Aero-elastic Tool Application to a Modern European Fighter

Modern Aero-elastic Tool Application to a Modern European Fighter J. Becker 1, M.H.L. Hounjet 2 and B.J.G. Eussen 3 1 EADS Deutschland GmbH Military Aircraft 81663 Munich, Germany e-mail: Juergen.Becker@m.eads.net 2 NLR Amsterdam National Aerospace Laboratory, NLR Anthony

More information

An Advanced Extensible Parametric Geometry Engine for Multi-Fidelity and Multi-Physics Analysis in Conceptual Design

An Advanced Extensible Parametric Geometry Engine for Multi-Fidelity and Multi-Physics Analysis in Conceptual Design An Advanced Extensible Parametric Geometry Engine for Multi-Fidelity and Multi-Physics Analysis in Conceptual Design Rob McDonald & David Marshall Cal Poly Andy Ko. JR Gloudemans NASA Glenn July 23, 2012

More information

Program: Advanced Certificate Program

Program: Advanced Certificate Program Program: Advanced Certificate Program Course: CFD-Vehicle Aerodynamics Directorate of Training and Lifelong Learning #470-P, Peenya Industrial Area, 4th Phase Peenya, Bengaluru 560 058 www.msruas.ac.in

More information

Improved Unsteady Aerodynamic Influence Coefficients for Dynamic Aeroelastic Response

Improved Unsteady Aerodynamic Influence Coefficients for Dynamic Aeroelastic Response Improved Unsteady Aerodynamic Influence Coefficients for Dynamic Aeroelastic Response Quinn Murphy Department of Mechanical Engineering McGill University Montréal, Canada December 212 A thesis submitted

More information

Introduction to C omputational F luid Dynamics. D. Murrin

Introduction to C omputational F luid Dynamics. D. Murrin Introduction to C omputational F luid Dynamics D. Murrin Computational fluid dynamics (CFD) is the science of predicting fluid flow, heat transfer, mass transfer, chemical reactions, and related phenomena

More information

INNOVATIVE CFD FOR SUPER-COMPUTER RESULTS ON YOUR DESKTOP

INNOVATIVE CFD FOR SUPER-COMPUTER RESULTS ON YOUR DESKTOP INNOVATIVE CFD FOR SUPER-COMPUTER RESULTS ON YOUR DESKTOP XFlow is a next generation CFD software that uses a proprietary, particle-based, meshless approach which can easily handle traditionally complex

More information

ONE DIMENSIONAL (1D) SIMULATION TOOL: GT-POWER

ONE DIMENSIONAL (1D) SIMULATION TOOL: GT-POWER CHAPTER 4 ONE DIMENSIONAL (1D) SIMULATION TOOL: GT-POWER 4.1 INTRODUCTION Combustion analysis and optimization of any reciprocating internal combustion engines is too complex and intricate activity. It

More information

Chapter 1: Introduction

Chapter 1: Introduction Chapter 1: Introduction This dissertation will describe the mathematical modeling and development of an innovative, three degree-of-freedom robotic manipulator. The new device, which has been named the

More information

CFD ANALYSIS OF ENGINE AIR INTAKE FOR A PUSHER TYPE LIGHT TRANSPORT AIRCRAFT

CFD ANALYSIS OF ENGINE AIR INTAKE FOR A PUSHER TYPE LIGHT TRANSPORT AIRCRAFT International Conference on Computer Aided Engineering (CAE-2013) Department of Mechanical Engineering, IIT Madras, India CFD ANALYSIS OF ENGINE AIR INTAKE FOR A PUSHER TYPE LIGHT TRANSPORT AIRCRAFT Vinay

More information

DETERMINATION OF FLIGHT STABILITY COEFFICIENTS USING A FINITE ELEMENT CFD

DETERMINATION OF FLIGHT STABILITY COEFFICIENTS USING A FINITE ELEMENT CFD DETERMINATION OF FLIGHT STABILITY OEFFIIENTS USING A FINITE ELEMENT FD harles R. O Neill Mechanical and Aerospace Engineering Oklahoma State University Stillwater, OK 7477 Abstract A 3D finite element

More information

The Nasuni Security Model

The Nasuni Security Model White Paper Nasuni enterprise file services ensures unstructured data security and privacy, enabling IT organizations to safely leverage cloud storage while meeting stringent governance and compliance

More information

Simulation of Aircraft Encounters with Perturbed Vortices Considering Unsteady Aerodynamic Effects

Simulation of Aircraft Encounters with Perturbed Vortices Considering Unsteady Aerodynamic Effects Simulation of Aircraft Encounters with Perturbed Vortices Considering Unsteady Aerodynamic Effects Berlin Institute of Technology Institute of Aeronautics and Astronautics, Flight Mechanics, Flight Control

More information

Innovative Fusion of Experiment and Analysis for Missile Design and Flight Simulation

Innovative Fusion of Experiment and Analysis for Missile Design and Flight Simulation Innovative Fusion of Experiment and Analysis for Missile Design and Flight Simulation Patrick H. Reisenthel, John F. Love, Daniel J. Lesieutre, and Marnix F. E. Dillenius Nielsen Engineering & Research,

More information

Introduction to Aerodynamic Shape Optimization

Introduction to Aerodynamic Shape Optimization Introduction to Aerodynamic Shape Optimization 1. Aircraft Process 2. Aircraft Methods a. Inverse Surface Methods b. Inverse Field Methods c. Numerical Optimization Methods Aircraft Process Conceptual

More information

314 JAXA Special Publication JAXA-SP E 2. WING TRACKING EXPERIMENTS The aim of the experiments is to isolate the wing geometry and kinematics wi

314 JAXA Special Publication JAXA-SP E 2. WING TRACKING EXPERIMENTS The aim of the experiments is to isolate the wing geometry and kinematics wi First International Symposium on Flutter and its Application, 2016 313 ANALYSIS OF KINEMATICS OF FLAPPING WING MAV USING OPTITRACK SYSTEMS Matthew NG Rongfa 1, Teppatat PANTUPHAG 2, Sutthiphong SRIGRAROM

More information

TOPOLOGY OPTIMIZATION OF WING RIBS IN CESSNA CITATION

TOPOLOGY OPTIMIZATION OF WING RIBS IN CESSNA CITATION TOPOLOGY OPTIMIZATION OF WING RIBS IN CESSNA CITATION [1],Sathiyavani S [2], Arun K K [3] 1,2 student, 3 Assistant professor Kumaraguru College of technology, Coimbatore Abstract Structural design optimization

More information

Improved High Frequency Dynamic Airframe Loads and Stress Prediction

Improved High Frequency Dynamic Airframe Loads and Stress Prediction Improved High Frequency Dynamic Airframe Loads and Stress Prediction Phillip Lang phillip.f.lang@boeing.com Technical Fellow The Boeing Company, Philadelphia, PA Dr. Louis Centolanza lcentolanza@aatd.eustis.army.mil

More information