An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
Subtitle: final report
By: Awatef Hamed, principal investigator.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-199439.
Publisher: University of Cincinnati; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Cincinnati, Ohio?]; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Corner flow.; Engine design.; Engine inlets.; Oblique shock waves.; Secondary flow.; Separated flow.; Shock wave interaction.; Supersonic inlets.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0187-M.

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