A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
By: by Scott Douglas Holland.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-188788.
Publisher: North Carolina State University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1991
Place of publication: Raleligh, NC; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Flow distribution.; Hypersonic inlets.; Inlet flow.; Supersonic combustion ramjet engines.; Three dimensional flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-0798-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 8  microfiches.