Transonic Reynolds Number and Leading-Edge Bluntness Effects on a 65° Delta Wing. | 東京工業大学附属図書館文献データベース

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Transonic Reynolds Number and Leading-Edge Bluntness Effects on a 65° Delta Wing.

Author(s):: Luckring, J.M.
Publication title:: AIAA paper
Title of ser.:: AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:: 2003
Pub. Year:: 2003
No.:: 2003-0753
Paper no.:: 2003-0753
Pages:: 12
Pub. info.:: American Institute of Aeronautics and Astronautics
ISSN:: 01463705
Language:: English
Call no.:: A07400
Type:: Technical Paper

Details

TDL ID:	ZA00001712
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	41st
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2003.01.06-2003.01.09
Note for article:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

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