Research Catalog

A numerical study of the effect of wake passing on turbine blade film cooling

Title
A numerical study of the effect of wake passing on turbine blade film cooling [microform] / James D. Heidmann.
Author
Heidmann, James D.
Publication
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; 107077
Subject
  • Computational fluid dynamics
  • Computational grids
  • Film cooling
  • Finite difference theory
  • Flow distribution
  • Gas turbine engines
  • Heat Transmission
  • Three dimensional flow
  • Turbine blades
  • Turbulent flow
  • Unsteady flow
  • Viscous flow
  • Wakes
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 96-0368-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:107077
OCLC
marcive35197508
Author
Heidmann, James D.
Title
A numerical study of the effect of wake passing on turbine blade film cooling [microform] / James D. Heidmann.
Imprint
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA technical memorandum ; 107077
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:107077
Research Call Number
READEX Microfiche NAS 1.15:107077
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