|
Technical Paper Sessions
|
|
|
Salle Guillaumet
|
Auditorium de Saint-Exupery
|
Spot
|
Salle Guillaumet
|
|
2:30 PM to 4:15 PM
|
1a- Stress Analysis
|
2a - Process Optimization & Improvement
|
3 - Rotor Dynamics
|
4-High Performance Computing
|
| 43 |
"A340-600 Fan Cowls
Finite Element Model: Using MSC.Nastran to Modelise CFC Secondary
Structure with Contact Boundary Conditions" EADS CASA
|
176 |
"Airbus and MSC.Software
Working Together on Structural Analysis" Airbus Deutschland
GmbH
|
16 |
"Procedure for Analyzing
Non-Axisymmetric Rotating Structures with MSC.Nastran" The
Boeing Company
|
35 |
"Maximizing MSC.Nastran
Multiprocessing Productivity on SGI" SGI & MSC.Software
Corporation
|
| 65 |
"MSC.Patran and FiberSIM:
An Integrated Solution for the Engineering of Composite Parts"
VISTAGY, Inc
|
10 |
"Rapid Design Iteration
Process for Spacecraft Kinematic Mounts Using Automatic Tet Meshing
and Global/Local Modeling Techniques" TRW Space & Technology;
MSC.Software Corporation
|
36 |
"Rotor Dynamic Analysis
Procedure" The Boeing Company
|
106 |
"The High Performance
Computing Division of MSC.Software" MSC.Software Corporation
|
| 77 |
"The Influence
of Material and Geometric Non-Linearity to Accuracy FEM Stress Analysis
of Landing Gear" Brno University of Technology
|
15 |
"Integration
of External Design Criteria for MSC.Nastran Structural Analysis and
Optimization" Lockheed Martin Aeronautics Company; MSC.Software
Corporation
|
105 |
"Simulation
of Aircraft Engine Blade-Out Structural Dynamics" NASA Glenn
Research Center
|
114 |
"Innovative
Engineering Environments and Computer Technology" Hewlett-Packard
|
| 141 |
"Stress Analysis of
an Aero-Engine High Pressure Compressor Spool" Hellenic Aerospace
Industry
|
19 |
"Wing-Pre-Wing-Pre-Processor
in MSC.Patran" EADS Airbus GmbH; MSC.Software
|
|
|
123 |
"Itanium Performance:
Getting Past the Hype, Getting You Results Faster" Hewlett-Packard
Corporation
|
| 164 |
"Stability Analysis
of Stiffened Panels Analytical and Finite Element Methods" Pechiney
|
44 |
"Automated Analysis
Process of Small Size Antennas with MSC.Nastran for Windows"
MEDIA Consultores de Ingenieria S.L.
|
|
|
178 |
"Performance Highlights of
the POWER4 Microprocessor for CAE Appllications" IBM Corporation |
|
4:15 PM to 4:45 PM
|
Break |
|
4:45 PM to 6:30 PM
|
1b-Stress Analysis
|
2b - Process Optimization & Improvement
|
5a - Dynamics
|
6a- Crash Impact
|
|
|
107
|
"A Case of Microgravity Analysis
on JEM by Introducing Reduced Matrix Models" Mitsubishi Space
Software Co., Ltd.
|
61
|
"Integrating the Design Process"
INBIS Group plc
|
6
|
"An Approach to Properly Account
for Structural Damping, Frequency-Dependent Stiffness/Damping, and
to Use Complex Matrices in Transient Response" MSC.Software
Corporation
|
7 |
"Impact Simulations of the Composite
Helicopter Structure with MSC.Dytran" Eurocopter Deutschland
GmbH
|
| 145 |
"Structural Analysis of Aeronautical
Components from MSC.Nastran Integrated Finite Element Models Management
to Specific Detailed Stressing" AXS - Analyse de Structures |
71 |
"Analysis Throughout the Development
Phase Using Superelements" Kongsberg Defense & Aerospace
|
17 |
"An Overview and Comparison of OTM
Formulations on the Basis of the Mode Displacement and Mode Acceleration
Method" ESA/ESTEC
|
18 |
"Lear Fan II Crash Test Simulation"
Lockheed Martin
|
| 161 |
"Prediction and Testing (ASTM E-837-89)
of Residual Stresses in Structures Caused by Welding" NASA;
Saudi Aramco Oil Company |
76 |
"Development of a New Generation
Aircraft for Pilot Training" Brno University of Technology
|
26 |
"Probabilistic Modal Response Analysis
for Turbine Engine Blade Design Using MSC.Nastran" Air Force
Research Laboratory
|
81 |
"Small Debris Impact Simulation Using
MSC.Dytran - Part II" EMBRAER
|
| |
|
158 |
"CATIA Analysis V5. Status and Strategy
for Easy and Fast Design - Analysis Optimization" Dassault
Systemes
|
34 |
"Rail Launch Missile Simulation Using
MSC.Nastran" MBDA Inc.
|
118 |
""Thrust Bearing Damage Simulation
and Redesign Investigation Using MSC.Dytran" Hamilton Sundstrand,
The United Technologies Corporation
|
| |
|
|
|
|
|
54 |
"Validation of Post-Buckling Behaviour
of Unstable Cross-Section Structures Under Compression-Loads" Industria
de Turbopropulsores, S.A. |
| |
|
|
|
|
|
180 |
"Effective Bird - FOD and Containment Analysis. MSC.Dytran
Simulation" Pratt & Whitney |
|
After Hours
|
|
6:30 PM to 8:30 PM
|
Cocktails in the exhibit area |
|
|
|
Tuesday April 9th, 2002
|
|
Keynote Speakers, Auditorium de SAINT-EXUPERY
|
|
9:00 AM to 9:30 AM
|
Hugo Resende, New Technologies Manager,
EMBRAER
|
|
9:30 AM to 10:15 AM
|
Sam Venneri, Associate
Admistrator for Aerospace Technology, NASA |
|
10:15 AM-10:45 AM
|
Jose Maria Alapont, President of Delphi
Automotive Systems Europe, Middle-East and Africa and Vice President
Delphi Automotive
|
|
10:45 AM to 11:15 AM
|
Break |
|
Technical Paper Sessions
|
|
|
Salle Guillaumet
|
Auditorium de Saint-Exupery
|
Spot
|
Salle Guillaumet
|
|
11:15 AM to 1:00 PM
|
6 - Thermal Analysis
|
7- Adding Engineering Value
|
5- Dynamics
|
8a- JSF
|
| 32 |
"Thermal Analysis of Fairchild
Dornier 728Jet Wing/Fuselage Interface Using MSC.Patran Thermal"
Fairchild Dornier GmbH
|
80 |
"The Implementation of MSC.Enterprise
Mvision at Embraer: History, Environment, Databases and Future Projects"
Embraer
|
46 |
"Modal Indentification of Quasi-Symmetric
Structures with an Example Taken From Aeroplanes Airframe Models"
vMACH Engineering; P+Z Engineering; University Krakow
|
|
| 58 |
"Thermo-Mechanical Analysis of
Airplane Carbon-Carbon Brakes Using MSC.Marc" MSC.Software
Corporation; The Institute of Aviation Warsaw, Poland; Warsaw Polytechnic
|
86 |
"The MSC.Software Simulation Data
Management Initiative" MSC.Software Corporation
|
50 |
"Design and Certification of Modifications
in Military Rotorcraft" TEGRAF Ingenieria
|
| 70 |
"MSC.Marc - ATAS: Advanced Thermal
Analysis Software for Modeling of Rocket Motors and Other Thermal
Protection Systems" Snecma Moteurs; CSSI; MSC.Software Corporation
|
153 |
"Robust Design: The Future of Engineering
Analysis in Design" MSC.Software Corporation; Phoenix Integration
|
55 |
"Vibroacoustic Analysis Procedure
to Obtain Forces and Stresses on Aerospace Structures" MEDIA
Consultores de Ingenieria S.L.; EADS CASA Espacio
|
| 149 |
"Component Modes Synthesis Applied
to a Thermal Transient Analysis of a Turbine Disc." Politecnico
di Torino; MSC.Software; Fiat Avio
|
177 |
"Integrated Conceptual and Preliminary
Design Environments Supporting Rapid Design Explorations and MDO"
MSC.Software Corporation |
82 |
"A New Method for Calculation of
Friction Grip Joints Subjected to Random Loads" Instituto
Nacional de Tecnica Aeroespacial
|
| 174 |
"Improving the Accuracy of Thermal
Analysis by Means of Fluid - Structure Coupling" AVL
|
172 |
"MSC.Software: How to Deliver Software
Services System" Fiat-Avio and MSC.Software |
9 |
"Finite Element Analysis of Ball Grid
Arrays Subjected to Random Vibration Tests" Raytheon Surveillance
& Reconnaisance Systems |
|
1:00 PM to 2:30 PM
|
Lunch |
|
2:30 PM to 4:15 PM
|
9-The Next Engineer
|
10a-Manufacturing Process
|
5c-Dynamics
|
8b- JSF
|
| |
"A new Internet will
be his engine and smart agents will help optimize tools and speed
problem solving. Web mentors, integrated information will fuel productivity
gains." MSC.Software Corporation
|
5 |
"Accurate FEA Prediction
of Extrusion Forming to Improve Aircraft Design and Manufacturing"
The Boeing Company
|
88 |
"Finite Element Method
Analysis and Life Estimation of Aircraft Structure Fatigue/Fracture
Critical Area" KAI (Korea Aerospace Industries)
|
|
| |
|
29 |
"Simulation of Welding
Using MSC.Marc" Volvo Aero Corporation, Luleaa University
of Technology
|
142 |
"Chaos and Uncertainty:
Fighting the Stagnation in CAE" MSC.Software Corporation
|
| |
|
52 |
"Application of the
Model of Stresses in the FE-Based Fracture Analysis in Cold and Semi-Hot
Forging" University of the German Federal Armed Forces Hamburg
|
163 |
"A New Loading Integration
Tool for MSC.Nastran in the Structural Development of the New AerMacchi
Trainer Aircraft" AerMacchi
|
| |
|
60 |
"Application of MSC.Marc
to the Prediction of Welding Residual Stresses" QinetiQ Ltd.;
MSC.Software Corporation
|
165 |
"A Statistical Method
of Determining Global Buckling Modes on the Chinook Helicopter Fuselage"
The Boeing Company; MSC.Software Corporation
|
| |
|
75 |
"Integration of the
Segmented Chip Forming in High Speed Cutting Process" University
of the German Federal Armed Forces Hamburg
|
|
|
| |
|
|
|
|
|
|
4:15 PM to 4:45 PM
|
Break |
|
4:45 PM to 6:30 PM
|
2c-Process Optimization
|
10b - Manufacturing Process
|
12-High Performance Computing
|
13a-Aerolasticity/Flightloads
|
| 97 |
"Support Structure of the AMS Permanent
Magnet in the Event of Complete Glue Failure" China Academy
of Launching Technology
|
89 |
"Stretch Forming Analysis for the
Skin of Aircraft, Model B717-200" Korean Air Company
|
68 |
"Optimized I/O for MSC.Nastran on
Compaq's Alpha Systems" Compaq Computer Corporation
|
131 |
"The Aerodynamic Prediction of an
Elastic Launch Vehicle" Orbital Sciences Corporation
|
| 124 |
"Results Post Processing Using MSC.Acumen"
MSC.Software Corporation; Snecma Moteurs
|
117 |
"Numerical Simulation of the SuperPlastic
Forming Process of the EFA-2000 Undercarriage Door" Alenia
Aerospazio; MSC.Software Italia
|
121 |
"Advanced Visualization Tools for
MSC.Software Products" CEI (Computational Engineering International)
|
159 |
"CATIA ELFINI AEROLASTICITY, Support
of Loads and Dynamics Processes from Concept to Operations" Dassault
Systemes
|
| 137 |
"FEM Application for Development
of ALH Airframe, Tailboom and Empennage" Rotary Wing Research
& Design Centre, Hindustan Aeronautics Limited
|
127 |
"Formulation of Intermediate Layer
Laws for Advanced Simulation Models of Precision Forging" Institute
for Metal Forming & Metal Forming Machine Tools
|
168 |
"High Performance Computing Supporting
Manufacturing Trends" Intel Corporation
|
|
|
| 139 |
"Global Integration and Management
of 21st Century Military Aircraft Development" Lockheed Martin
|
132 |
"3D Modelisation of Thermo-Mechano-Metallurgical
Coupling During Welding Process Assisted by MSC.Marc" Universite
de Technologie de Compiegne; EADS CCR
|
179 |
"SUN HPC update" Sun Microsystems,
Inc. |
|
|
| 148 |
"Productivity Improvement Through
the Usage of Software Tools with the Illustration of a Case Study"
Aircraft Research & Design Centre, Hindustan Aeronautics Limited
|
147 |
"Improvements of FE-Analysis in
Cold, Warm and Hot Forging Processes" Institute for Metal
Forming & Metal Forming Machine Tools
|
|
|
|
|
| |
|
|
|
|
|
|
|
|
After Hours
|
|
6:30 PM
|
Transportation departs to Dinner |
|
7:00 PM to 8:30 PM
|
Dinner |
| |
|
|
Wednesday April 10, 2002
|
|
Keynote Speakers
|
|
9:00 AM to 9:45 AM
|
Sergio Salvano, Turbo
Machinery Design Manager, Fiat Avio |
|
9:45 AM to 10:30 AM
|
Dr. C. G. Krishnadas Nair, Chairman,
Hindustan Aeronautics of India |
|
10:30 AM to 11:00 AM
|
Dr. Frank Baetke, HP Global HPC-Technology
Program Manager, HP |
|
11:00 AM to 11:30 AM
|
Break |
|
Technical Paper Sessions
|
|
|
Salle Guillaumet
|
Auditorium de Saint Exupery
|
Spot
|
Salle Guillaumet
|
|
11:30 AM to 1:15 PM
|
14a - Composite Material
|
15- Fatigue
|
16a-Structural Optimization
|
13b- Aerolasticity/Flightloads
|
| 28 |
"A Hierarchic 3D Finite Element
for Laminated Composites" German Aerospace Center, Institute
of Structural Mechanics
|
24 |
"Development of a New Method and
Software for Durability Analysis of Structures with Account of Nonlinear
Effects Linked to Multicomponent Loading on Example of GTE Structures
Analysis and on the Basis of MSC.Software Systems Applications"
Lyulka-Saturn, Inc.
|
1 |
"Optimization of a Simple Aircraft
Wing Model" Fibraforte Engenharia
|
14 |
"An Improved Process for Mapping
Aeroelastic Loads Across Structural Meshes" MSC.Software Corporation
|
| 30 |
"Efficient Transverse Stress Calculation
and Failure Prediction in Arbitrarily Curved Shell-Structures Using
TRAVEST" German Aerospace Center, Institute of Structural
Mechanics
|
27 |
"High Performance Fracture Approach
to Fatigue Crack Analysis & Life Prediction" SENER
|
22 |
"Response Surface Generation with
Minimum Evaluation Points Using Sensitivity Information" Air
Force Research Laboratory
|
51 |
"3D Aerodynamic Models Adaptation
for MSC.Nastran" Sukhoi Design Bureau
|
| 40 |
"Automated Three-Dimensional Finite
Element Modelling of Composite Aircraft Bolted Joints - Modelling
Issues" University of Limerick
|
112 |
"Advanced Simulation Techniques
for the Coupled Fatigue - NVH Optimization of Engines" MSC.Software
Corporation
|
39 |
"Structural Optimization of Helicopter
Empennage Using MSC.Nastran" The Boeing Company
|
|
|
| 41 |
"Initial Multi-Bolt Joint Results
from BOLJAT, a Tool for Semi-Automated Three-Dimensional Modelling
of Composite Aircraft Bolted Joints" University of Limerick
|
171 |
"Durability Prediction Using Automatic
Crack Growth Simulation" Computational Mechanics
|
42 |
"Fully Stressed Design in MSC.Nastran"
MSC.Software Corporation
|
|
|
| |
|
|
|
156 |
"Economical Model Variation by Means
of Dedicated Base-Driven Tests" LMS International |
|
|
|
1:15 PM to 2:45 PM
|
Lunch
|
|
2:45 PM to 4:30 PM
|
14b -Composite Material
|
18-Modeling
|
16b-Structural Optimization
|
13c-Aerolasticty/Flightloads
|
| 136 |
"Stress Concentration and Stability
Studies in Compostie Ribs with Flanged Cutouts" Infosys Technologies,
Ltd.
|
104 |
"Presentation of Parametric Model
of A380 Engine Pylon with MSC.Patran" EADS Airbus SA
|
72 |
"Propulsion Structure Modeling and
Analysis Rapid Tool" The Boeing Company
|
31 |
"Integration of MSC.Flightloads
and Dynamics at Lockheed Martin Aeronautics Company" Lockheed
Martin; MSC.Software Corporation
|
| 138 |
"Evolving Composites Simulation
Requirements and Solutions" MSC.Software Corporation
|
|
|
94 |
"PATRAN/COMPASS: A Multidisciplinary
Design Tool for Aeronautical Structures" Aircraft Strength
Research Institute of China
|
102 |
"Advanced CFD Analysis of External
Aerodynamics Using CFX" AEA Technology GmbH
|
| 150 |
"Development of a Structural Component
with Composite Materials. Numerical Analysis, Technologies and Prototyping"
Consorzio CETMA
|
155 |
"Acoustic Analysis Using Finite
and Infinite Element: Development of an ACTRAN Preference in MSC.Patran"
Free Field Technologies S.A.
|
122 |
"Application of Structural Optimisation
to Airbus Engine and Pylon Designs" EADS Airbus France
|
135 |
"A Comparison Between the Aerodynamic
Pressure Factoring and the Aerodynamic Derivatives Factoring Methods
for the Doublet Lattice Program" EMBRAER
|
| 151 |
"Structural Analysis of an Automotive
Cockpit Cross Car-Beam Using MSC.Nastran" Delphi Automotive
|
160 |
"Aerospace Use Cases with CATIA
V5" Dassault Systemes
|
129 |
"Upcoming Performance Enhancements
in MSC.Nastran When Performing Very Large Scale NVH Design Sensitivity
and Optimization Tasks" Cray Inc; MSC.Software Corporation
|
157 |
"Numerical Life Prediction of a Slat Track Under Test Flight Conditions" LMS International; ASCO Industries; Vrije Universiteit Brussel |
| |
|
167 |
"Development of a New Simulation
Software for Visual Ergonomy of a Cockpit" OPTIS; NEMOPTIC;
IMNSSA
|
166 |
"Developments and Applications of
NAPAO for Optimum Design of Aerospace Structures" Alenia Aerospazio;
Politecnico di Torino
|
|
|
| |
|
|
|
175 |
"Interface Between MSC.Nastran and
FAIPA, An Interior Point Algorithm for Optimal Design" Fibraforte
Engenharia
|
|
|
|
