Effect of coolant temperature and mass flow on film cooling of turbine blades
By: Vijay K. Garg and Raymond E. Gaugler.
Contributors: Gaugler, Raymond E.; United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 112760.; NASA technical memorandum -- 112760.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1997
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Turbine blades.; Stagnation temperature.; Stagnation pressure.; Rotors.; Hole distribution (Mechanics); Film cooling.; Compressibility.
Notes: Shipping list no.: 98-0818-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.