Static Aeroelastic Analysis of Supersonic Experimental Airplane NEXST-1 Flight Test

Static Aeroelastic Analysis of Supersonic Experimental Airplane NEXST-1 Flight Test

著者名:

H. Kawakami ( Japan Aerospace Exploration Agency, Mitaka, Japan )
T. Takatoya
H. Ishikawa ( Sanko Software Development Company, Ltd., Shinjuku, Japan )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Applied Aerodynamics Conference

シリーズ巻号:

2007

発行年:

2007

通号:

2007-4174

ペーパー番号:

AIAA Paper 2007-4174

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200714 [CD-ROM 2007 Disc 14]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049503
シリーズID:	PA00000157
会議名:	AIAA Applied Aerodynamics Conference
回次:	25th
会議開催地:	Miami, Florida
会議開催年:	2007.06.25-2007.06.28
論文注記:	25th AIAA Applied Aerodynamics Conference, Miami, Florida, June 25-28, 2007

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1 テクニカルペーパー Static Aeroelastic Analysis of Experimental SST NEXST-1 Flight Test Using Wing-Body Configuration Model H. Kawakami, T. Takatoya, H. Ishikawa American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Validation of CFD Capability for Supersonic Transport Analysis Using NEXST-1 Flight Test Results M. Umeda, K. Takenaka, K. Hatanaka, D. Hirayama, W. Yamazaki, K. Matsushima,, K. Nakahashi American Institute of Aeronautics and Astronautics
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