Research Catalog

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Title
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 [microform] / Scott D. Holland.
Author
Holland, Scott D.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Details

Additional Authors
Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 109152
Alternative Title
Wind tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
Subject
  • Actuators
  • Blocking
  • Cowlings
  • Engine inlets
  • Hypersonic inlets
  • Hypersonic wind tunnels
  • Inlet flow
  • Shock wave interaction
  • Supersonic combustion ramjet engines
  • Wind tunnel tests
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0276-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:109152
OCLC
marcive32777874
Author
Holland, Scott D.
Title
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 [microform] / Scott D. Holland.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
Series
NASA technical memorandum ; 109152
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.
Added Author
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:109152
Research Call Number
READEX Microfiche NAS 1.15:109152
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