Research Catalog

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

Title
Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.
Author
Garg, Vijay Kumar, 1938-
Publication
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Gaugler, Raymond E.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; 106954
Subject
  • Film cooling
  • Heat transfer coefficients
  • Temperature distribution
  • Turbine blades
  • Velocity distribution
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 96-0021-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:106954
OCLC
marcive33973275
Author
Garg, Vijay Kumar, 1938-
Title
Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.
Imprint
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA technical memorandum ; 106954
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Gaugler, Raymond E.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:106954
Research Call Number
READEX Microfiche NAS 1.15:106954
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