Research Catalog

Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface

Title
Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface [microform] / V.P. Maksimov and A.A. Maslov.
Author
Maksimov, V. P.
Publication
Washington, D.C. : National Aeronautics and Space Administration, [1983]

Details

Additional Authors
  • Maslov, A. A.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; NASA TM-77341
Uniform Title
NASA technical memorandum ; 77341.
Subject
  • Boundary layer control
  • Supersonic wind tunnels
  • Boundary layer transition
  • Flow stability
  • Surface cooling
  • Wall temperature
  • Wind tunnel nozzles
  • Wind tunnel walls
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.15:77341
OCLC
marcive236165318
Author
Maksimov, V. P.
Title
Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface [microform] / V.P. Maksimov and A.A. Maslov.
Imprint
Washington, D.C. : National Aeronautics and Space Administration, [1983]
Series
NASA technical memorandum ; NASA TM-77341
NASA technical memorandum ; 77341.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1984]. 1 microfiche.
Added Author
Maslov, A. A.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:77341
Research Call Number
GPO Microfiche NAS 1.15:77341
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