Sonic Boom Reduction Using an Adjoint Method for Wing-Body Configurations in Supersonic Flow

Sonic Boom Reduction Using an Adjoint Method for Wing-Body Configurations in Supersonic Flow

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. 2

通号:

2002-5547

ペーパー番号:

AIAA-2002-5547

開始ページ:

1326

終了ページ:

1335

総ページ数:

10

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.2)

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001459
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

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1 テクニカルペーパー An Adjoint Method Method for the Calculation of Remote Sensitivities in Supersonic Flow Nadarajah, S., Jameson, A., Alonso, J. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Active Flutter Control using an Adjoint Method K. Palaniappan, P. Sahu, J. Alonso, A. Jameson American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Design Optimization of High- Lift Configurations Using a Viscous Continuous Adjoint Method Kim, S., Alonso, J.J., Jameson, A. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー A gradient accuracy study for the adjoint-based navier-stokes design method Kim, S., Alonso, J.J., Jameson, A. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Sonic Boom Reduction via Remote Inverse Adjoint Approach S. Nadarajah, O. Soucy, C. Balloch American Institute of Aeronautics and Astronautics	9 テクニカルペーパー A Gradient Accuracy Study for the Adjoint-Based Navier-Stokes Design Method Kim, S., Alonso, J. J., Jameson, A. American Institute of Aeronautics and Astronautics
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5 テクニカルペーパー Optimal Control of Unsteady Flows Using a Time Accurate Method Nadarajah, S., Jameson, A. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction J. Lee, A. Jameson American Institute of Aeronautics and Astronautics
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