Transonic Flutter Simulation for Wing-Pylon-Nacelle Configuration Using Navier-Stokes Equations

Transonic Flutter Simulation for Wing-Pylon-Nacelle Configuration Using Navier-Stokes Equations

著者名:

H. Arizono ( Japan Aerospace Exploration Agency, Mitaka, Tokyo, Japan )
H. Kheirandish ( Research Center of Computational Mechanics Inc., Shinagawa, Tokyo, Japan )
J. Nakamichi ( Japan Aerospace Exploration Agency, Tokyo, Japan )
H. Morino ( Mitsubishi Heavy Industries, Ltd., Nagoya, Japan )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

シリーズ巻号:

2008

発行年:

2008

通号:

2008-1897

ペーパー番号:

AIAA Paper 2008-1897

出版情報:

Reno, Nevada: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200803 [CD-ROM 2008 Disc 3]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049521
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
回次:	49th
会議開催地:	Schaumburg, IL
会議開催年:	2008.04.07-2008.04.10
論文注記:	49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 7-10 April 2008, Schaumburg, IL

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