Drag Minimization Through the use of Mission Adaptive Trailing Edge Flaps and Fuel State Control

Drag Minimization Through the use of Mission Adaptive Trailing Edge Flaps and Fuel State Control

著者名:

Zink, S. ( Lockheed Martin Aeronautics Company, Ft.Worth, TX )
Love, M.
Youngren, H. ( AeroCraft Consulting, Portland, ME )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Multidisciplinary Analysis and Optimization Conference

シリーズ巻号:

10th

発行年:

2004

通号:

2004-4365

ペーパー番号:

AIAA Paper 2004-4365

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200417 [CD-ROM 2004 Disc 17]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001557
シリーズID:	PA00000051
会議名:	AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
回次:	10th
会議開催地:	Albany, New York
会議開催年:	2004.08.30-2004.09.01

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