Optimization Using Variable Fidelity Solvers: Exploration of an Approximation Management Framework for Aerodynamic Shape Optimization

Optimization Using Variable Fidelity Solvers: Exploration of an Approximation Management Framework for Aerodynamic Shape Optimization

著者名:

掲載資料名:

A collection of technical papers : 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, 4-6 September 2002

シリーズ名:

AIAA Paper : Symposium on Multidisciplinary Analysis and Optimization

シリーズ巻号:

2002

発行年:

2002

巻:

v. 3

通号:

2002-5595

ペーパー番号:

AIAA-2002-5595

開始ページ:

1794

終了ページ:

1802

総ページ数:

9

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475504 [1563475502]

言語:

英語

請求記号:

A07400/025400 (v.3)

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001460
シリーズID:	PA00000159
会議名:	AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
回次:	9th
会議開催地:	Atlanta, Georgia
会議開催年:	2002.09.04-2002.09.06

類似資料:

1 テクニカルペーパー Distributed Optimizations Using Optimal Solution Sensitivity C. Tribes, J. Trépanier American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Flexible transonic wing design optimization with discipline-oriented decompositions J. Dallaire, C. Tribes, J. Trépanier American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Airfoil Shape Optimization Using NURBS Representation Under Thickness Constraint Painchaud-Ouellet, S., Tribes, C., Trepanier, J., Pelletier, D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Integration and Multidisciplinary Design Optimization of a Simplified Gas Turbine Modeling Using Perl and iSIGHT Turcotte, J., Trepanier, J., Tribes, C., Panchenko, Y., Dion, M., Plante, G. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Airfoil Generation and Optimization using Multiresolution B-Spline Control with Geometrical Constraints N. Giammichele, J. Trépanier, C. Tribes American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Multiobjective Composite Material Design using the Variable Fidelity Model Management Optimization Framework Mejía-Rodríguez, Gilberto, Renaud, John E, Tomar, Vikas American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Propagation of Uncertainties in a Multilevel Vehicle Model Using Evidence Theory A. Chokri, J. Trépanier, C. Tribes, P. Fenyes, X. Gu American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Convergence Using Variable Fidelity Approximation Data in a Trust Region Managed Augmented Lagrangian Approximate Optimization Rodriguez,J., Renaud,J., Watson,L. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Characterizing Global Behavior of Approximation Functions J. Bourgeois, J. Trepanier, F. Guibault, C. Tribes American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Aerodynamic Optimisation of Modern Transport Wing using Efficient Variable Fidelity Shape Parameterisation A. Morris, C. Allen, T. Rendall American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Decomposition of Multidisciplinary Optimization Problem: Formulations and Application to a Simplified Wing Design Tribes, C., Dube, J., Trepanier, J. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー A Framework for Parallel High-Fidelity Aerodynamic and Aeroelastic Optimization A. Morris, C. Allen, T. Rendall American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12