Research Catalog

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

Title
Mach 10 computational study of a three-dimensional scramjet inlet flow field [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, 1995]

Details

Additional Authors
Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 4602
Subject
  • Aerodynamics
  • Computational fluid dynamics
  • Computational grids
  • Hypersonic speed
  • Inlet flow
  • Navier-Stokes equation
  • Shock wave interaction
  • Supersonic combustion ramjet engines
  • Supersonic inlets
  • Three dimensional flow
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0478-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4602
OCLC
marcive32851835
Author
Holland, Scott D.
Title
Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA technical memorandum ; 4602
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4602
Research Call Number
READEX Microfiche NAS 1.15:4602
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