Research Catalog

Boundary layer transition in the leading edge region of a swept cylinder in high speed flow

Title
Boundary layer transition in the leading edge region of a swept cylinder in high speed flow [microform] / Colin P. Coleman.
Author
Coleman, Colin P.
Publication
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]

Details

Additional Authors
  • Ames Research Center.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA/TM ; 1998-112224
Uniform Title
NASA technical memorandum ; 112224.
Subject
  • Boundary layer transition
  • Leading edges
  • Wind tunnel tests
  • Reynolds number
  • Swept wings
  • Supersonic flow
Note
  • Shipping list no.: 99-0685-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:112224
OCLC
marcive41964744
Author
Coleman, Colin P.
Title
Boundary layer transition in the leading edge region of a swept cylinder in high speed flow [microform] / Colin P. Coleman.
Imprint
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
Series
NASA/TM ; 1998-112224
NASA technical memorandum ; 112224.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 3 microfiches.
Added Author
Ames Research Center.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:112224
Research Call Number
READEX Microfiche NAS 1.15:112224
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