Applicability of an Analytical Shock/Expansion Solution to the Elevon Control Effectiveness for a 2-D Hypersonic Vehicle Configuration

Applicability of an Analytical Shock/Expansion Solution to the Elevon Control Effectiveness for a 2-D Hypersonic Vehicle Configuration

著者名:

T. Skujins ( University of Michigan, Ann Arbor, MI )
C. Cesnik
M. Oppenheimer ( Air Force Research Laboratory, Dayton, OH )
D. Doman

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

シリーズ巻号:

2008

発行年:

2008

通号:

2008-6384

ペーパー番号:

AIAA 2008-6384

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200810 [CD-ROM 2008 Disc 10]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050905
シリーズID:	PA00000162
会議名:	AIAA Atmospheric Flight Mechanics Conference and Exhibit
回次:	2008
会議開催地:	Honolulu, HI
会議開催年:	2008.08.18-2008.08.21

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