Optimal airfoil and blade design in compressible and incompressible flows

Optimal airfoil and blade design in compressible and incompressible flows

著者名:

Medic, G. ( INRIA Rocquencourt )
Mohammadi, B. ( Universite de Montpellier and INRIA Rocquencourt )
Moreau, S. ( VALEO Thermique Moteur )
Stanciu, M. ( INRIA Rocquencourt )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA Fluid Dynamics Conference

シリーズ巻号:

1998

発行年:

1998

通号:

98-2898

ペーパー番号:

98-2898

開始ページ:

1

終了ページ:

9

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:	ZA00050855
シリーズID:	PA00000147
会議名:	AIAA Fluid Dynamics Conference
回次:	29th
会議開催地:	Albuquerque, NM
会議開催年:	1998.06.15-1998.06.18
論文注記:	29th AIAA Fluid Dynamics Conference, June 15-18, 1998/Albuquerque, NM

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1 テクニカルペーパー 3D Optimal Shape Design for Complex Flows: Application to Turbomachinery Medic, G., Mohammadi, B., Petruzzelli, N., Stanciu, M., Hecht, F. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Use of a flow analogy in solving compressible and incompressible flows Darbandi, M., Schneider, G.E. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー 3D optimal shape design for complex flows : application to turbomachinery Medic, G., Mohammadi, B., Petruzzelli, N., Stanciu, M., Hecht, F. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Optimum Shape Design Using Automatic Differentiation in Reverse Mode Hafez, M., Mohammadi, B., Pironneau, O. National Aeronautics and Space Adminstration
3 テクニカルペーパー Optimal control of 3D turbulent flow over circular cylinder Medic, G., Mohammadi, B. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Effect of Blade Design at Equal Loading on Broadband Noise Y. Rozenberg, M. Roger, S. Moreau American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Optimal Control of 3D Turbulent Flow over Circular Cylinder Medic, G., Mohammadi, B. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Optimal shape design, reverse mode of automatic differentiation and turbulence Mohammadi, B. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Solving Compressible Flow Using SIMPLE Incompressible Procedure Darbandi,M., Schneider,G.E., Hosseinizadeh,S.F. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Prediction of airfoil noise in compressible turbulent flows Guidati, G., Wagner, S. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Nonlinear development of cross-flow instabilitites in compressible and incompressible boundary layer flows Gajjar, J.S.B., Arebi, M.A., Sibanda, P. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Effect of Airfoil Aerodynamic Load on Trailing Edge Noise Moreau, S., Roger, M., Iaccarino, G. American Institute of Aeronautics and Astronautics

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