Research Catalog

Shock-tunnel combustor testing for hypersonic vehicles

Title
  1. Shock-tunnel combustor testing for hypersonic vehicles [microform] / Mark Loomis.
Published by
  1. San Jose, Calif. : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
Author
  1. Loomis, Mark.

Details

Additional authors
  1. United States. National Aeronautics and Space Administration.
Description
  1. 1 v.
Series statement
  1. NASA contractor report ; NASA CR-196836
  2. MCAT Institute final report ; 94-07
Alternative title
  1. Shock tunnel combustor testing for hypersonic vehicles
Subject
  1. Wind tunnel tests
  2. Air breathing engines
  3. Combustion chambers
  4. Engine tests
  5. Hypersonic aircraft
  6. Hypersonic flow
  7. Hypersonic inlets
  8. Hypersonic speed
  9. Inlet nozzles
  10. Mach number
  11. Propulsion system configurations
  12. Propulsion system performance
  13. Supersonic combustion ramjet engines
  14. Two dimensional flow
Call number
  1. READEX Microfiche NAS 1.26:196836
Note
  1. Distributed to depository libraries in microfiche.
  2. Shipping list no.: 95-0068-M.
Reproduction (note)
  1. Microfiche.
Author
  1. Loomis, Mark.
Title
  1. Shock-tunnel combustor testing for hypersonic vehicles [microform] / Mark Loomis.
Imprint
  1. San Jose, Calif. : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
Series
  1. NASA contractor report ; NASA CR-196836
  2. MCAT Institute final report ; 94-07
Reproduction
  1. Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.
Added author
  1. United States. National Aeronautics and Space Administration.
Gpo item no.
  1. 0830-H-14 (MF)
Sudoc no.
  1. NAS 1.26:196836
Research call number
  1. READEX Microfiche NAS 1.26:196836
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