A Parametric Experimental Study for Momentum Transfer by Plasma Actuator

A Parametric Experimental Study for Momentum Transfer by Plasma Actuator

著者名:

T. Abe ( Japan Aerospace Exploration Agency, Kanagawa, Japan )
Y. Takizawa
S. Sato
N. Kimura ( Tokai University, Kanagawa, Japan )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2007

発行年:

2007

通号:

2007-0187

ペーパー番号:

AIAA Paper 2007-187

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200701 [CD-ROM 2007 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050739
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	45th
会議開催地:	Reno, Nevada
会議開催年:	2007.01.08-2007.01.11

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2 テクニカルペーパー Acoustic Wave Analysis for a DBD Plasma Actuator T. Abe, S. Sato, K. Taguchi, Y. Tamura American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Experiment on Shock Layer Enhancement by Electro-Magnetic Effect in Reentry-Related High-Enthalpy Flow Takizawa, Y., Matsuda, A., Sato, S., Abe, T., Konigorski, D. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Optical Observation of Discharge Plasma Structure in DBD Plasma Actuator Y. Takizawa, A. Matsuda, K. Kikuchi, A. Sasoh, T. Abe American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Experimental and Numerical Study on Performance of Extendible Nozzle for Altitude Compensation M. Sato, T. Kimura, S. Moriya, M. Tadano, T. Masuoka, M. Yoshida American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Experimental Study on Drag Enhancement in Electrodynamic Heat Shield for a Blunt Body in a Weakly Ionized Plasma Flow M. Kawamura, A. Matsuda, H. Katsurayama, H. Otsu, D. Konigorski, S. Sato, T. Abe American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Momentum coupling and flow induction in a DBD plasma actuator Abe, Takashi, Takagaki, Masahiko American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Electro-Magnetic Effect on Shock Layer Structure in Reentry-Related High-Enthalpy Flow Takizawa, Y., Sato, S., Abe, T., Konigorski, D. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Momentum Transfer for an Aerodynamic Plasma Actuator with an Imposed Boundary Layer J. Baughn, C. Porter, B. Peterson, T. McLaughlin, C. Enloe, G. Font, C. Baird American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Experimental Study of Nonequilibrium Phenomena Behind Strong Shock Waves Generared in Super-Orbital Reentry Flight. Matsuda, A., Fujita, K., Sato, S., Abe, T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Electro-Magnetic Effect on Reentry-Related High-Enthalpy Flow Takizawa, Y., Matsushita, K., Sato, S., Fujita, K., Abe, T., Konigorski, D. American Institute of Aeronautics and Astronautics

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