Research Catalog

Mach 10 computational study of a three-dimensional scramjet inlet flow field

Title
  1. Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.
Published by
  1. Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Author
  1. Holland, Scott D.

Details

Additional authors
  1. Langley Research Center.
Description
  1. 1 v.
Series statement
  1. NASA technical memorandum ; 4602
Subject
  1. Aerodynamics
  2. Computational fluid dynamics
  3. Computational grids
  4. Hypersonic speed
  5. Inlet flow
  6. Navier-Stokes equation
  7. Shock wave interaction
  8. Supersonic combustion ramjet engines
  9. Supersonic inlets
  10. Three dimensional flow
Call number
  1. READEX Microfiche NAS 1.15:4602
Note
  1. Distributed to depository libraries in microfiche.
  2. Shipping list no.: 95-0478-M.
Reproduction (note)
  1. Microfiche.
Author
  1. Holland, Scott D.
Title
  1. Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.
Imprint
  1. Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
  1. NASA technical memorandum ; 4602
Reproduction
  1. Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added author
  1. Langley Research Center.
Gpo item no.
  1. 0830-D (MF)
Sudoc no.
  1. NAS 1.15:4602
Research call number
  1. READEX Microfiche NAS 1.15:4602
View in legacy catalog