Effect of velocity and temperature distribution at the hole exit 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 technical memorandum -- 106954.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0021-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.