Numerical simulation of supersonic flow using a new analytical bleed boundary condition
By: G.J. Harloff and G.E. Smith.
Contributors: Smith, G. E.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 198368.; NASA contractor report -- NASA CR-198368.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer control.; Computational fluid dynamics.; Flow distribution.; Oblique shock waves.; Shock wave interaction.; Supersonic boundary layers.; Supersonic flow.; Supersonic inlets.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0232-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.