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. ( NASA Langley Research Center )

Publication title:

NASA Technical Reports

Pub. Year:

1996

Vol.:

19970006702

Issue:

NASA-TM-111790

Pt.:

NAS 1.15:111790

Page(from):

1

Page(to):

18

Pages:

18

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001434

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