Generalized vortex lattice method for oscillating lifting surfaces in planar supersonic flow

Generalized vortex lattice method for oscillating lifting surfaces in planar supersonic flow

著者名:

Soviero, Paulo A. ( Instituto Tecnologico de Aeronautica, Brazil )
Resende, Hugo B.

掲載資料名:

A collection of technical papers : 14th AIAA Applied Aerodynamics Conference, June 17-19, 1996, New Orleans, LA

シリーズ名:

AIAA Paper : AIAA Applied Aerodynamics Conference

シリーズ巻号:

CP965

発行年:

1996

巻:

pt. 2

通号:

96-2491

ペーパー番号:

AIAA 96-2491

開始ページ:

886

終了ページ:

894

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472121 [1563472120]

言語:

英語

請求記号:

(pt.1)A07400/962667,(pt.2)A07400/962668

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00006873
シリーズID:	PA00000157
会議名:	AIAA Applied Aerodynamics Conference
回次:	14th
会議開催地:	New Orleans, LA
会議開催年:	1996.06.17-1996.06.19

類似資料:

1 テクニカルペーパー Unsteady Aerodynamic Coefficients Obtained by a Compressible Vortex Lattice Method F. Hernandes, P. Soviero American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Hypersonic Panel Flutter in a Rarefied Atmosphere Resende, Hugo B. National Aeronautics and Space Adminstration
2 テクニカルペーパー NONPLAMAR VORTEX LATTICE METHOD FOR ANALYSIS OF COMPLEX MULTIPLE LIFTING SURFACES Rajeswari, B. National Aeronautics and Space Administration	8 テクニカルペーパー A Reaction Force Measurement Study of the Transition of an In-Line Vortex to Slug Flow B. de Witt, R. Hugo American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Compressible Unsteady Vortex Lattice Method for Arbitrary Two Dimensional Motion of Thin Profiles P. Soviero, F. Hernandes American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Analysis of Compressible Potential Flow Over Airfoils Using the Dual Reciprocity Method A. Cavalieri, P. Soviero American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Control surface effects on tail flutter Resende, Hugo B., Nakagawa, Nelson M., Kamiyama, Mauro T. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー LIFTING-SURFACE THEORY OF OSCILLATING PROPELLERS IN COMPRESSIBLE FLOW Ichikawa, Teruo National Aeronautics and Space Administration
5 テクニカルペーパー ANALYSIS OF WINGS WITH LEADING EDGE AND OR TRAILING EDGE SEGMENTED (SPANWISE) FLAPS USING PLANAR HORSE SHOE VORTEX LATTICE METHOD Rajeswari, B. National Aeronautics and Space Administration	11 テクニカルペーパー Optical Contouring of an Acrylic Surface for Pipe-Flow Visualization Experiments B. de Witt, H. Coronado-Diaz, R. Hugo American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Numerical Study Of Vortex Flows Around A Supersonic Transport High-Lift Configuration With Forebody Control Surfaces D. Yeh, R. Clark American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Flow Simulation Around an Airfoil Using Lattice Boltzmann Method on Generalized Coordinates Imamura, T., Yoshida,M., Suzuki,K., Nakamura,T. American Institute of Aeronautics and Astronautics

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