Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
By: V.K. Garg, R.E. Gaugler.
Contributors: Gaugler, R. E.; United States. National Aeronautics and Space Administration.
Series: NASA/TM -- 208146.; NASA technical memorandum -- 208146.
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: Velocity distribution.; Temperature distribution.; Turbine blades.; Film cooling.; Hole geometry (Mechanics); Coolants.
Notes: Shipping list no.: 99-0354-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.