Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade
By: David Rosenbaum
Contributors: 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
Series: NASA technical paper -- 1603; AVRADCOM technical report -- 79-34
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 53
Subjects: Turbines -- Blades; Jets -- Fluid dynamics -- Data processing; Heat -- Transmission -- Computer programs
Notes: "Propulsion Laboratory, AVRADCOM Research and Technology Laboratories, Lewis Research Center."

Distributed to depository libraries in microfiche

"January 1980"--Cover

STAR category 34

Includes bibliographical references