Research Catalog

Effect of coolant temperature and mass flow on film cooling of turbine blades

Title
Effect of coolant temperature and mass flow on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.
Author
Garg, Vijay Kumar, 1938-
Publication
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

Details

Additional Authors
  • Gaugler, Raymond E.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA-TM ; 112760
Uniform Title
NASA technical memorandum ; 112760.
Subject
  • Turbine blades
  • Stagnation temperature
  • Stagnation pressure
  • Rotors
  • Hole distribution (Mechanics)
  • Film cooling
  • Compressibility
Note
  • Shipping list no.: 98-0818-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:112760
OCLC
marcive39783354
Author
Garg, Vijay Kumar, 1938-
Title
Effect of coolant temperature and mass flow on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.
Imprint
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
NASA-TM ; 112760
NASA technical memorandum ; 112760.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
Gaugler, Raymond E.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:112760
Research Call Number
READEX Microfiche NAS 1.15:112760
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