Boundary Layer Calculations for Preliminary Design of Wings in Supersonic Flow

Boundary Layer Calculations for Preliminary Design of Wings in Supersonic Flow

著者名:

掲載資料名:

A collection of technical papers : 17th AIAA Applied Aerodynamics Conference, Norfolk, Virginia 28 June-1 July, 1999

シリーズ名:

AIAA Paper : AIAA Applied Aerodynamics Conference

シリーズ巻号:

1999

発行年:

1999

通号:

99-3104

ペーパー番号:

AIAA-99-3104

開始ページ:

47

終了ページ:

57

総ページ数:

11

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472985 [1563472988]

言語:

英語

請求記号:

A07400/993100

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00000089
シリーズID:	PA00000157
会議名:	AIAA Applied Aerodynamics Conference
回次:	17th
会議開催地:	Norfolk, VA
会議開催年:	1999.06.28-1999.07.01

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2 テクニカルペーパー Natural Laminar Flow for Quiet and Efficient Supersonic Aircraft. Kroo, I., Sturdza, P., Tracy, R., Chase, J. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー THE DESIGN AND PRELIMINARY CALIBRATION OF A BOUNDARY-LAYER FLOW CHANNEL Rao, Dhanvada M. et al. National Aeronautics and Space Administration
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