Physical Study of Shock-Wave / Boundary-Layer Interaction Control in Transonic Flow

Physical Study of Shock-Wave / Boundary-Layer Interaction Control in Transonic Flow

著者名:

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:

2000

発行年:

2000

通号:

2000-0933

ペーパー番号:

00-0933

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:	ZA00050874
シリーズID:	PA00000138
会議名:	AIAA Aerospaces Science Meeting and Exhibit
回次:	38th
会議開催地:	Reno, NV
会議開催年:	2000.01.10-2000.01.13
論文注記:	38th Aerospace Sciences Meeting & Exhibit 10-13 January 2000 / Reno, NV

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1 テクニカルペーパー Study of passive control in a transonic shock wave/boundary layer interaction Bur, R., Corbel, B., Delery, J. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Passive Control of Oblique Shock/Boundary Layer Interaction at High Mach Number Borovoy, V., Gusev, V., Skuratov, A., Stolyarov, E., Delery, J., Chanetz, B. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Experimental Study of Transonic Interaction with Shock and Boundary-Layer Control Bur, R., Corbel, B. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Active Control of Shock/Boundary Layer Interaction in Transonic Flow Over Airfoils Vadillo, J., Agarwal, R., Hassan, A. American Institute of Aeronautics and Astronautics
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