Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler.

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Bibliographic Details
Main Author:	Garg, Vijay Kumar, 1938-
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Gaugler, R. E.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1997]
Series:	NASA technical memorandum ; 208146.
Subjects:	Velocity distribution. Temperature distribution. Turbine blades. Film cooling. Hole geometry (Mechanics) Coolants.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:208146
NAS 1.15:208146	Restricted Place a Hold