Research Catalog

Inlet flowfield investigation.

Title
Inlet flowfield investigation. Part II.. Computation of the flow about a supercruise forebody at supersonic speeds [microform].
Publication
Seattle, Wash. : Boeing Military Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]

Details

Additional Authors
  • Boeing Military Airplane Company.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA contractor report ; 172315
Alternative Title
Computation of the flow about a supercruise forebody at supersonic speeds
Subject
  • Aerodynamics, Supersonic
  • Jet engines > Air intakes
  • Computational fluid dynamics
  • Flow distribution
  • Forebodies
  • Inlet flow
  • Navier-Stokes equation
  • Supersonic flow
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.26:172315
OCLC
marcive182721494
Title
Inlet flowfield investigation. Part II.. Computation of the flow about a supercruise forebody at supersonic speeds [microform].
Imprint
Seattle, Wash. : Boeing Military Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
Series
NASA contractor report ; 172315
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 2 microfiches.
Added Author
Boeing Military Airplane Company.
Langley Research Center.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:172315
Research Call Number
GPO Microfiche NAS 1.26:172315
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