Effect of fin leading edge sweep on shock-shock interaction at Mach 6
By: Scott A. Berry and Robert J. Nowak.
Contributors: Nowak, Robert J.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 111790.
Publisher: American Institute of Aeronautics and Astronautics; [National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Leading edge sweep.; Shock wave interaction.; Wind tunnel tests.; Hypersonic speed.; Reynolds number.
Notes: Shipping list no.: 98-0007-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.