Swept-Wing Laminar Flow Control Studies Using Cessna O-2A Test Aircraft

Swept-Wing Laminar Flow Control Studies Using Cessna O-2A Test Aircraft

著者名:

M. Martin ( Northrop Grumman Corporation, Palmdale, CA )
A. Carpenter ( Texas A&M University, College Station, TX )
W. Saric

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : U.S. Air Force T&E Days

シリーズ巻号:

2008

発行年:

2008

通号:

2008-1636

ペーパー番号:

AIAA Paper 2008-1636

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200802 [CD-ROM 2008 Disc 2]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049520
シリーズID:	PA00000047
会議名:	U.S. Air Force T&E Days
回次:	2008
会議開催地:	Los Angels, CA
会議開催年:	2008.02.05-2008.02.07
論文注記:	U.S. Air Force T&E Days, 5-7, February 2008, Los Angels, California

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