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Program For Wednesday, 10-Sep-2008
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0800 - 0900 |
Flight Test of the Blended Wing Body X-48B
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Lecture Theatre |
| Keynote Speaker: Dr. Robert Liebeck, Senior Fellow, The Boeing Company, Huntington Beach, CA |
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| Session
1-
MAO-1
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Advanced and Innovative Approximation Methods
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Colwood |
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Chaired by: D. STRONG, U.S. Air Force Research Laboratory, Dayton, OH
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0900
AIAA-2008-5800
Large- Scale Multidisciplinary Validation of Enriched Multipoint Cubic Approximations
R. Roberts and R. Canfield, Air Force Institute of Technology, Wright-Patterson AFB, OH
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0930
AIAA-2008-5801
A Comparison of Four Approximation Techniques for An Euler Based Induced Drag Function
R. Kolonay, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; R. Roberts, Air Force Institute of Technology, Wright-Patterson AFB, OH; and L. Lambe, Multidisciplinary Software Systems Research Corporation, Bloomingdale, IL
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1000
AIAA-2008-5802
Design and Analysis of Computer Experiments in Multidisciplinary Design Optimization: A Review of How Far We Have Come - Or Not
T. Simpson, The Pennsylvania State University, University Park, PA; V. Toropov, University of Leeds, Leeds, Great Britain; V. Balabanov, The Boeing Company, Seattle, WA; and F. Viana, University of Florida, Gainesville, FL
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1030
AIAA-2008-5803
Adaptive and Parallel Capabilities in the Multipoint Approximation Method
A. Polynkin and V. Toropov, University of Leeds, Leeds, West Yorkshire, Great Britain; S. Shahpar, Rolls-Royce plc, Derby, Great Britain
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| Session
2-
MAO-2
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Aerodynamic Shape Optimization I
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View Royal |
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Chaired by: A. STRIZ, University of Oklahoma, Norman, OK, and C. LIERSCH, German Aerospace Center (DLR), Brunswick, Germany
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0900
AIAA-2008-5806
A Newton- Krylov Approach for Aerodynamic Shape Optimization of Wings
T. Leung and D. Zingg, University of Toronto, Toronto, Ontario, Canada
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0930
AIAA-2008-5807
An Investigation of Induced Drag Minimization Using a Newton- Krylov Algorithm
J. Hicken and D. Zingg, Institute for Aerospace Studies University of Toronto, Toronto, Ontario, Canada
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1000
AIAA-2008-5808
A Strategy for Multi- Objective Shape Optimization for Turbine Stages in Three- Dimensional Flow
M. Arabnia and W. Ghaly, Concordia University, Montreal, Quebec, Canada
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1030
AIAA-2008-5809
Inlet Shape Optimization Based on POD Model Reduction of the Euler Equations
J. Goss and K. Subbarao, University of Texas at Arlington, Arlington, TX
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1100
AIAA-2008-5810
Helicopter Rotor Design Using a Time- Spectral and Adjoint- Based Method
S. Choi, Stanford University, Stanford, CA; M. Potsdam, U.S. Army Aeroflightdynamics Directorate, Moffett Field, CA; K. Lee, G. Iaccarino, and J. Alonso, Stanford University, Stanford, CA
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1130
AIAA-2008-5811
Sensitivity Analysis Using Direct Differentiation and Adjoint Vector Methods for Helicopter Rotor Flow In Hover
A. Dumont, A. Le Pape and J. Peter, Office National d'Etudes et Recherches Aerospatiales, Meudon, France; S. Huberson, LEA, Futuroscope-Chasseneuil, France
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| Session
3-
MAO-3
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Applied Optimization
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Sidney |
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Chaired by: N. ALEXANDROV, NASA Langley Research Center, Hampton, VA
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0900
AIAA-2008-5812
Fuzzy Optimal Algorithms for an Optimal Swarm of Autonomous Aircrafts
Z. Richards and R. Salters, Denver University, Denver, CO
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0930
AIAA-2008-5813
Designing Straight- Bladed Vertical Axis Wind Turbine Using the Cascade Theory
M. Islam and A. Fartaj, University of Windsor, Windsor, Ontario, Canada; M. Amin, Montana State University, Bozeman, MT; R. Carriveau, University of Windsor, Windsor, Ontario, Canada
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1000
AIAA-2008-5814
Toward Optimal Transport Networks
N. Alexandrov, NASA Langley Research Center, Hampton, VA; R. Kincaid and E. Vargo, College of William & Mary, Williamsburg, VA
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1030
AIAA-2008-5815
Trajectory Planning for Hydraulically Actuated Flexible Loader Crane
M. Ebbesen, T. Andersen and M. Hansen, Aalborg University, Aalborg, Jutland, Denmark
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1100
AIAA-2008-5816
Strategic Sequential Redesign for the Creation of Families of Systems
M. Chamberlain, Dynamic Concepts Inc., Huntsville, AL; J. Allen and F. Mistree, Georgia Institute of Technology, Savannah, GA
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| Session
4-
MAO-4
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Design Methods I
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Oak Bay 1 |
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Chaired by: A. NAIM, University at Buffalo, Buffalo, NY, and M. BLAIR, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
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0900
AIAA-2008-5818
A Framework for Formulating Design Problems in a System- of- Systems Context
S. Ayyalasomayajula, D. Fry and D. DeLaurentis, Purdue University, West Lafayette, IN
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0930
AIAA-2008-5819
Product Family Design: Combined Modular and Scalable Platforms using Concurrent Smart Pareto Filter
J. Yearsley and C. Mattson, Brihgam Young University, Provo, UT
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1000
AIAA-2008-5821
A Review of MDO Methods to Optimize for Energy Efficiency
D. Moorhouse, D. Paul, and D. Pratt, Air Force Research Laboratory, Wright-Patterson AFB, OH
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1030
AIAA-2008-5823
A Study on Changing Requirements Part Way Through an Aerodynamic Design Process
J. Jarrett, University of Cambridge, Cambridge, Great Britain
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| Session
5-
MAO-5
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Design Under Uncertainty: Applications I
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Esquimalt |
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Chaired by: P. ROHL, Advatech Pacific Inc, Redlands, CA
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0900
AIAA-2008-5824
Probabilistic Analysis and Design of a Raked Wing Tip for a Commercial Transport
B. Mason, T. Chen, S. Padula, J. Ransom and W. Stroud, NASA Langley Research Center, Hampton, VA
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0930
AIAA-2008-5826
Risk Analysis in Lifecycle Costing of Aluminium
X. Tan, J. Wang, Y. Xu, R. Curran and S. Raghunathan, Queen's University Belfast, Belfast, Great Britain; D. Gore, Airbus UK, Bristol, Great Britain
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1000
AIAA-2008-5827
Non- Deterministic Shape Optimization in Aeronautics
J. Pons-Prats, Serra Aeronautics, Barcelona, Spain; E. Oñate, F. Zárate, and G. Bugeda, CIMNE UPC, Barcelona, Spain; and J. Hurtado, UNC, Manizales, Colombia
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1030
AIAA-2008-5828
Robust Design Optimisation of Gas Turbine Compression Systems
T. Ghisu, G. Parks, J. Jarrett and P. Clarkson, University of Cambridge, Cambridge, Great Britain
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1100
AIAA-2008-5829
Multi- Objective Optimization Under Uncertainty of Satellite Systems Via Simulated Annealing
M. Magnin, Nanyang Technological University, Singapore, Singapore; D. Thunnissen, Space Systems/Loral, Palo Alto, CA; and S. Au, City University of Hong Kong, Hong Kong, China (prc)
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| Session
6-
MAO-6
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MA&O Applications: Aero Systems Analysis
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Oak Bay 2 |
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Chaired by: M. STELMACK, Lockheed Martin Aeronautics Company, Palmdale, CA
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|
0900
AIAA-2008-5830
Three- Dimensional Multi- Objective UAV Path Planner Using Meta- Paths for Decision Making and Visualization
L. Swartzentruber, J. Foo and E. Winer, Iowa State University, Ames, IA
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0930
AIAA-2008-5832
Environmental MDO and Uncertainty Hybrid Approach Applied to a Supersonic Business Jet
Y. Deremaux, N. Pietremont, J. Negrier, E. Herbin and M. Ravachol, Dassault Aviation, Saint Cloud, France
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1000
AIAA-2008-5833
Optimization of Control Strategy and Key Components of a Two- mode Hybrid Vehicle
Y. Zhou, J. Wishart, A. Younis and Z. Dong, University of Victoria, Victoria, British Columbia, Canada
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1030
AIAA-2008-5835
An Optimal Approach to Unmanned Maritime Surveillance Analysis
M. Wilkins and T. Marchelli, Northrop Grumman Corporation, San Diego, CA
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| Session
7-
MAO-7
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MA&O Applications: Structures I
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Saanich 2 |
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Chaired by: A. MESSAC, Rensselaer Polytechnic Institute, Troy, NY
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0900
AIAA-2008-5836
Coupling MDO and Principal Component Analysis techniques for Model Updating and Damage Detection
S. Ricci and M. Terraneo, Politecnico di Milano, Milano, Italy
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0930
AIAA-2008-5838
Modeling and Optimization of a Laser Shock Peening Process
G. Singh and R. Grandhi, Wright State University, Dayton, OH; D. Stargel and K. Langer, AFRL/RBSM, Wright-Patterson AFB, OH
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1000
AIAA-2008-5839
Topology Optimization of Structures Subjected to High- Cycle Load Conditions
M. Mrzyglod, Cracow University of Technology, Cracow, Poland
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1030
AIAA-2008-5840
Advanced PRSEUS Structural Concept Design and Optimization
V. Li and A. Velicki, The Boeing Company, Huntington Beach, CA
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| Session
8-
MAO-8
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MDO Algorithms
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Saanich 1 |
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Chaired by: J. MARTINS, University of Toronto, Toronto, ON, and S. TOSSERAMS, Eindhoven University of Technology, Eindhoven, The Netherlands
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0900
AIAA-2008-5841
Enhanced Collaborative Optimization: Application to an Analytic Test Problem and Aircraft Design
B. Roth and I. Kroo, Stanford University, Stanford, CA
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0930
AIAA-2008-5842
Survey of Modeling and Optimization Strategies for High- Dimensional Design Problems
S. Shan, University of Manitoba, Winnipeg, Manitoba, Canada; G. Wang, Simon Fraser University, Surrey, BC, Canada
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1000
AIAA-2008-5843
Extension of Analytical Target Cascading Using Augmented Lagrangian Coordination for Multidisciplinary Design Optimization
S. Tosserams, L. Etman and J. Rooda, Eindhoven University of Technology, Eindhoven, The Netherlands; M. Kokkolaras, The University of Michigan, Ann Arbor, MI
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1030
AIAA-2008-5845
A Robust Homotopy Method for Equality Constrained Nonlinear Optimization
X. Bai, J. Turner, and J. Junkins, Texas A&M University, College Station, TX
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1200 - 1330 |
Student Paper Competition Poster Session
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| Session
9-
MAO-9
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Aircraft Optimization
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Saanich 1 |
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Chaired by: F. ENGELSEN, The Boeing Company, Seattle, WA, and G. KENNEDY, University of Toronto, Toronto, Canada
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1330
AIAA-2008-5847
Aerostructural Optimization of Aircraft Structures Using Asymmetric Subspace Optimization
G. Kennedy, J. Martins, and J. Hansen, University of Toronto, Toronto, Canada
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1400
AIAA-2008-5849
Scaling for a Static Nonlinear Response of a Joined- Wing Aircraft
V. Bond, 716th Test and Evaluation Squadron, Arnold Air Force Base, TN; R. Canfield, Air Force Institute of Technology, Wright-Patterson AFB, OH; J. Cooper, University of Liverpool, Liverpool, Great Britain; and M. Blair, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
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1430
AIAA-2008-5848
Stochastic Gust Analysis Techniques for Aircraft Conceptual Design
K. Fidkowski, University of Michigan, Ann Arbor, MI; I. Kroo, Stanford University, Stanford, CA; K. Willcox, Massachusetts Institute of Technology, Cambridge, MA; and F. Engelson, The Boeing Company, Seattle, WA
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| Session
10-
MAO-10
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Computational Methods
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Sidney |
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Chaired by: P. ZINK, Lockheed Martin Corporation, Benbrook, TX
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1330
AIAA-2008-5853
Trends, Features, and Tests of Common and Recently Introduced Global Optimization Methods
A. Younis, Z. Dong, and J. Gu, University of Victoria, Victoria, Canada; and G. Li, College of Mechanical and Automobile Engineering, Hunan University, Hunan, China (prc)
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1400
AIAA-2008-5855
Accelerating Design Optimization Via Principal Components Analysis
T. Ghisu, G. Parks, J. Jarrett and P. Clarkson, University of Cambridge, Cambridge, Great Britain
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1430
AIAA-2008-5856
Reducing Computational Effort of the Normal Constraint Method by Eliminating Redundant Optimization Runs a Priori
N. Boyce and C. Mattson, Brihgam Young University, Provo, UT
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1500
AIAA-2008-5857
Adjoint- Based Methodology for Time- Dependent Optimization
N. Yamaleev, North Carolina A&T State University, Greensboro, NC; B. Diskin, National Institute of Aerospace, Hampton, VA; E. Nielsen, NASA Langley Research Center, Hampton, VA
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| Session
11-
MAO-11
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Design Methods II
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Oak Bay 1 |
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Chaired by: J. RENAUD, University of Notre Dame, Notre Dame, IN
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1330
AIAA-2008-5859
Advantages and Disadvantages of a Simultaneously Coupled Least- Squares Finite Element Formulation for Fluid- Structure Interaction
C. Rasmussen and R. Canfield, Air Force Institute of Technology, Wright-Patterson AFB, OH; and J. Reddy, Texas A&M University, College Station, TX
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1400
AIAA-2008-5861
Optimization of a Scramjet Fuel Injection Array: An Application of Mixed Variable Generalized Pattern Search with Kriging Surrogates
B. Sparkman and J. Chrissis, Air Force Institute of Technology, Wright-Patterson AFB, OH; M. Gruber, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; and M. Abramson, The Boeing Company, Seattle, WA
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1430
AIAA-2008-5863
Sensitivity Analysis of a Strongly Coupled Aero- Structural System Using Direct and Adjoint Methods
M. Marcelet, J. Peter, and G. Carrier, Office National d'Etudes et Recherches Aerospatiales, Chatillon, France
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1500
AIAA-2008-5864
The Quadratic Mode Method for Fluid- Structure Coupling of High Aspect Ratio Wing
K. Jung, ADD, Daejeon, South Korea; J. Lee and J. Kwon, KAIST, Daejeon, South Korea; I. Kang, ADD, Daejeon, South Korea
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| Session
12-
MAO-12
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Design Under Uncertainty: Applications II
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Esquimalt |
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Chaired by: P. BERAN, Air Force Research Laboratory, Wright-Patterson AFB, OH
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1330
AIAA-2008-5865
Optimal Design of Constrained- Layer Damping Considering Variability in Material and Operational Condition
D. Lee, Dongeui University, Busan, South Korea; B. Jung and B. Youn, University of Maryland, College Park, MD
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1400
AIAA-2008-5866
Simultaneous Buckling and Fundamental Frequency Optimization of Frames Under Uncertain Loadings
A. Ferreira and A. De Faria, Instituto Tecnológico de Aeronáutica, São José dos Campos, Brazil
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1430
AIAA-2008-5867
Improvement of Airfoil Performances Under Multi Uncertainties Modeled by Tensorial- Expanded Chaos Collocation
V. Pediroda, L. Parussini, and C. Poloni, University of Trieste, Trieste, Italy; and S. Parashar, ESTECO North America, Livonia, MI
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1500
AIAA-2008-5868
Uncertainty of Composite Wing Aeroelastic Behaviour
A. Manan and J. Cooper, University of Liverpool, Liverpool, Great Britain
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1530
AIAA-2008-5869
Optimization of Laminated Composite Plates with Reliability Constraints
P. Gosling and F. Faimun, Newcastle University, Newcastle-Upon-Tyne, Great Britain; and O. Polit, University Paris X, Paris, France
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| Session
13-
MAO-13
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MA&O Applications: Aerodynamics
|
Oak Bay 2 |
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Chaired by: M. STELMACK, Lockheed Martin Aeronautics Company, Palmdale, CA
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1330
AIAA-2008-5871
Viscous Optimization of Interacting Lifting Surfaces
V. Chapin and Y. Caumel, ISAE, Toulouse, France; and R. Neyhousser, Aquitaine Design Team, Arcachon, France
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1400
AIAA-2008-5872
Improved Representation of High Lift Devices for a Multidisciplinary Preliminary Aircraft Design Process
C. Werner-Westphal, W. Heinze and P. Horst, Technische Universitaet Braunschweig, Brunswick, Germany
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1430
AIAA-2008-5873
Multiobjective Hypersonic Entry Aeroshell Shape Optimization
J. Theisinger and R. Braun, Georgia Institute of Technology, Atlanta, GA
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1500
AIAA-2008-5874
A New Airfoil for the Supporting Struts of Smaller- Capacity Straight- Bladed VAWT
M. Islam and A. Fartaj, University of Windsor, Windsor, Ontario, Canada; M. Amin, Montana State University, Bozeman, MT; D. Ting, University of Windsor, Windsor, Ontario, Canada
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1530
AIAA-2008-5875
Optimization of a Scaled Sensorcraft Model with Passive Gust Alleviation
J. Cooper, University of Liverpool, Liverpool, Great Britain; S. Miller, University of Manchester, Manchester, Great Britain; O. Sensburg, Cranfield University, Cranfield, Great Britain; and G. Vio, University of Liverpool, Liverpool, Great Britain
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1600
AIAA-2008-5876
A Multidisiplinary Code Coupling Approach for Analysis and Optimization of Aeroelastic Systems
M. Nikbay, L. Oncu, and A. Aysan, Istanbul Technical University, Istanbul, Turkey
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| Session
14-
MAO-14
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MA&O Applications: Structures II
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Saanich 2 |
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Chaired by: V. TOROPOV, University of Leeds, Leeds, Great Britain
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1330
AIAA-2008-5877
An Alternative View on Weight Estimation for the Aircraft Industry: Problems and MDO Solutions
C. Hannon, L. Agyepong, V. Toropov and O. Querin, University of Leeds, Leeds, Great Britain
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1400
AIAA-2008-5878
Structural Optimization of the Landing Gear of a Mini- UAV
B. Tugay and H. Türkmen, Istanbul Technical University, Istanbul, Turkey
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1430
AIAA-2008-5879
Reliability Based Design Optimization of a Composite Airframe Component
S. Patnaik, Ohio Aerospace Institute, Brook Park, OH; S. Pai and R. Coroneos, NASA Glenn Research Center, Cleveland, OH
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1500
AIAA-2008-5880
Topology Optimization for the Attenuation of Flow Induced Vibration of a Plate
F. Lau, CCTAE, Lisbon, Portugal; A. Gomes, IDMEC, Lisbon, Portugal
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| Session
15-
MAO-15
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MDO Methodologies
|
Lecture Theatre |
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Chaired by: A. STRIZ, University of Oklahoma, Norman, OK, and A. NAIM, University at Buffalo, Buffalo, NY
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|
1330
AIAA-2008-5883
Optimum Launch Vehicle Fairing: An MDO Approach
M. Colonno and J. Alonso, Stanford University, Stanford, CA
|
1400
AIAA-2008-5885
Optimization of Nonlinear Structural Responses with MD Nastran
S. Zhang, E. Johnson, and D. Chou, MSC Software Corporation, Santa Ana, CA; G. Park, Hanyang University, Ansan City, South Korea; and L. Proctor, MSC Software Corporation, Santa Ana, CA
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1430
AIAA-2008-5886
Issues When Selecting Naval Ship Configurations from a Pareto- Optimal Set
B. van Oers, Delft University of Technology, Delft, The Netherlands; D. Stapersma, Royal Netherlands Naval College, Den Helder, The Netherlands; and H. Hopman, Delft University of Technology, Delft, The Netherlands
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1500
AIAA-2008-5888
Global Optimization Algorithms in Multidisciplinary Design Optimization
D. Peri, INSEAN - Italian Ship Model Basin, Roma, Italy; G. Fasano, University Ca' Foscari of Venice, Venice, Italy; D. Dessi and E. Campana, INSEAN - Italian Ship Model Basin, Roma, Italy
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| Session
16-
MAO-16
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Surrogate Modeling and Applications
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Colwood |
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Chaired by: M. KOKKOLARAS, University of Michigan, Ann Arbor, MI, and S. KODIYALAM, Silicon Graphics Inc., Sunnyvale, CA
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1330
AIAA-2008-5889
Surrogate- Based Optimization of a Microfluidic Weir Structure for Single- Cell Manipulation
T. Robinson, B. Ooi, B. Taff, K. Willcox, and J. Voldman, Massachusetts Institute of Technology, Cambridge, MA
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1400
AIAA-2008-5890
Surrogate Modeling for Uncertainty Assessment with Application to Aviation Environmental System Models
D. Allaire and K. Willcox, Massachusetts Institute of Technology, Cambridge, MA
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1430
AIAA-2008-5891
A Hybridized Self- Organizing Response Surface Methodology
R. Moral and G. Dulikravich, Florida International University, Miami, FL
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1500
AIAA-2008-5892
A Hybrid RBF Based Method for Highly Multidimensional Response Surfaces Using Scarce Data Sets
M. Colaco, Military Institute of Engineering, Rio de Janeiro, Brazil; and G. Dulikravich, Florida International University, Miami, FL
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1530
AIAA-2008-5893
A Geostatistical Perspective for the Surrogate- Based Integration of Variable Fidelity Models
E. Nava, S. Pintos and N. Queipo, The University of Zulia, Maracaibo, Venezuela
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| Session
17-
MAO-17
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Topology Optimization Methods I
|
View Royal |
|
Chaired by: K. CHOI, University of Iowa, Iowa City, IA, and E. LUND, Aalborg University, Aalborg East, Denmark
|
|
1330
AIAA-2008-5895
Design of Porous Materials Using Topology Optimization
D. Bandyopadhyay, A. Benard and A. Diaz, Michigan State University, East Lansing, MI
|
1400
AIAA-2008-5896
A New Method for Design of Composite Structures for Strength and Stiffness
R. Lipton, Louisiana State University, Baton Rouge, LA; M. Stuebner, North Carolina State University, Raleigh, NC
|
1430
AIAA-2008-5897
Multi- Criteria Multi- Material Topology Optimization of Laminated Composite Structures
E. Lund, L. Johansen, C. Hvejsel, and E. Olesen, Aalborg University, Aalborg East, Denmark
|
1500
AIAA-2008-5898
Topology and Controller Parameter Optimization in Dynamic Mechatronic Systems
A. Albers, J. Ottnad, and J. Minx, University of Karlsruhe, Karlsruhe, Germany; and P. Haeussler, FE-Design GmbH, Karlsruhe, Germany
|
1530
AIAA-2008-5899
Topology Optimization for Force Sensor Structure based on Singular Value Decomposition
A. Takezawa, Hiroshima University, Higashihiroshima, Japan; S. Nishiwaki, Kyoto University, Kyoto, Japan; M. Kitamura, Hiroshima University, Higashi-Hiroshima, Japan; and E. Silva, Escola Politécnica da Universidade de São Paulo, São Paulo, Brazil
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|
1630 - 1730 |
Structure Analysis Contribution to Aircraft Multidisciplinary Optimization: Airbus Recent Examples and Perspectives
|
Lecture Theatre |
| Keynote Speaker: Dr. Jocelyn Gaudin, Structures Analysis Research Manager, Airbus, Toulouse, France |
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|
1800 - 1930 |
Welcome Reception
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