Research Catalog

A method for calculating turbulent boundary layers and losses in the flow channels of turbomachines

Title
A method for calculating turbulent boundary layers and losses in the flow channels of turbomachines [microform] / Lawrence F. Schumann.
Author
Schumann, Lawrence F.
Publication
[Washington, D.C. : National Aeronautics and Space Administration, 1987]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
[17] p. : ill.
Series Statement
  • NASA technical memorandum ; 88928
  • USAAVSCOM technical report ; 86-C-36
Uniform Title
  • NASA technical memorandum ; 88928.
  • AVSCOM technical report ; 86-C-36.
Subject
  • Channel flow
  • Diffusion
  • Turbomachinery
  • Turbulent boundary layer
  • Turbulent flow
Bibliography (note)
  • Includes bibliographical references (p. 6).
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.15:88928
OCLC
marcive639238499
Author
Schumann, Lawrence F.
Title
A method for calculating turbulent boundary layers and losses in the flow channels of turbomachines [microform] / Lawrence F. Schumann.
Imprint
[Washington, D.C. : National Aeronautics and Space Administration, 1987]
Series
NASA technical memorandum ; 88928
USAAVSCOM technical report ; 86-C-36
NASA technical memorandum ; 88928.
AVSCOM technical report ; 86-C-36.
Bibliography
Includes bibliographical references (p. 6).
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration]. 1987. 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration.
Other Form:
Paper version: Method for calculating turbulent boundary layers and losses in the flow channels of turbomachines. 17 p. (OCoLC)227696139
Online version: Schumann, Lawrence F. Method for calculating turbulent boundary layers and losses in the flow channels of turbomachines. (OCoLC)639241509
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:88928
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