Effects of sensitivity analysis on airfoil design

Effects of sensitivity analysis on airfoil design

著者名:

Eyi, S. ( Middle East Technical University )
Lee, K.D. ( University of Illinois )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

1998

発行年:

1998

通号:

98-0909

ペーパー番号:

98-0909

開始ページ:

1

終了ページ:

11

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050859
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	36th
会議開催地:	Reno, NV
会議開催年:	1998.01.12-1998.01.15
論文注記:	36th Aerospace Sciences Meeting & Exhibit, January 12-15, 1998/Reno, NV

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1 テクニカルペーパー Efficiency improvement in sensitivity evaluation in aerodynamic shape optimization Eyi, S., Lee, K.D. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー A Computational Investigation of Ice Geometry Effects on Airfoil Performances Shim,J., Chung,J., Lee,K.D. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Transonic turbomachinery blade design using optimization Eyi, S., Lee, K.D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Performances of numerical and analytical Jacobians in flow and sensitivity analysis Ezertas, A. A., Eyi, S. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Effects of Sensitivity Analysis on Turbomachinery Blade Design Kocabicak, E., Eyi, S. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Detailed Analysis of CG Variation Effect on Connecting Rod Design of a Turbocharged Diesel Engine. Nadaf, K.D., Joshi, S.G. Society of Automotive Engineers
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5 テクニカルペーパー Multi-element high-lift design using the Navier-Stokes equations Eyi, S., Chand, K.K., Lee, K.D., Rogers, S.E., Kwak, D. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Airfoil geometry and flow compressibility effects on wing and blade flutter Jones, K.D., Platzer, M.F. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Parallelized Design Optimization for Transonic Wings Using Aerodynamic Sensitivity Analysis Lee, B.J., Kim, C.S., Kim,C., Rho, O.H., Lee, K.D. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー An Efficient Aerodynamic Design Method Using Asymptotic Solutions of the Euler Equations. Shim, J., Lee, K.D., Verhoff, A. American Institute of Aeronautics and Astronautics

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