Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By: Scott D. Holland.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 109152
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Actuators; Blocking; Cowlings; Engine inlets; Hypersonic inlets; Hypersonic wind tunnels; Inlet flow; Shock wave interaction; Supersonic combustion ramjet engines; Wind tunnel tests
Other titles: Wind tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0276-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.