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] / V.K. Garg, R.E. Gaugler.
Author
Garg, V. K.
Publication
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

Details

Additional Authors
  • Gaugler, R. E.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA/TM ; 208146
Uniform Title
NASA technical memorandum ; 208146.
Subject
  • Velocity distribution
  • Temperature distribution
  • Turbine blades
  • Film cooling
  • Hole geometry (Mechanics)
  • Coolants
Note
  • Shipping list no.: 99-0354-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:208146
OCLC
marcive41168941
Author
Garg, V. K.
Title
Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler.
Imprint
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
NASA/TM ; 208146
NASA technical memorandum ; 208146.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Added Author
Gaugler, R. E.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:208146
Research Call Number
READEX Microfiche NAS 1.15:208146
View in Legacy Catalog