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Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade/

Main Author:	Rosenbaum, David
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Propulsion Laboratory U.S., Army Research and Technology Laboratories U.S. Structures Laboratory, Lewis Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Series:	NASA technical paper AVRADCOM technical report 1603
Subjects:	Turbines > Blades Jets > Fluid dynamics > Data processing Heat > Transmission

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