Effects of fin leading edge sweep on shock-shock interaction at Mach 6

Effects of fin leading edge sweep on shock-shock interaction at Mach 6

Author(s):

Berry, Scott A. ( NASA Langley Research Center )
Nowak, Robert J.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1996

Pub. Year:

1996

No.:

96-0230

Paper no.:

96-0230

Page(from):

1

Page(to):

14

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050843
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	34th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1996.01.15-1996.01.18
Note for article:	34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV

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