Numerical Study on Effect of a Thermal Bump in Supersonic Flow Control

Numerical Study on Effect of a Thermal Bump in Supersonic Flow Control

著者名:

H. Yan ( Wright State University, Dayton, OH )
D. Gaitonde ( U.S. Air Force Research Laboratory, Dayton, OH )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

シリーズ巻号:

2008

発行年:

2008

通号:

2008-3790

ペーパー番号:

AIAA Paper 2008-3790

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200807 [CD-ROM 2008 Disc 7]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050894
シリーズID:	PA00000148
会議名:	Plasmadynamics and Lasers Conference
回次:	39th
会議開催地:	Seattle, WA
会議開催年:	2008.06.23-2008.06.26
論文注記:	39th Plasmadynamics and Lasers Conference, 23-26 June 2008, Seattle, Washington

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1 テクニカルペーパー The Effect of a Thermal Bump in Supersonic Flow H. Yan, D. Gaitonde, J. Shang American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Control of Edney IV Interaction by Energy Pulse H. Yan, D. Gaitonde American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Supersonic Flow Control by Pulsed Thermal Bump H. Yan, D. Gaitonde, J. Shang American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Hypersonic Flow Control Utilizing Electromagnetic-Aerodynamic Interaction J. Shang, P. Huang,, H. Yan, S. Surzhikov, D. Gaitonde American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Effect of Thermally-Induced Surface Perturbation in Compressible Flow H. Yan, D. Gaitonde American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Investigation of Localized Arc Filament Plasma Actuator in Supersonic Boundary Layer H. Yan, D. Gaitonde, J. Shang American Institute of Aeronautics and Astronautics
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