Effects of film injection angle on turbine vane cooling
By: James W. Guantner.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper ; 1095; NASA technical paper -- 1095.
Publisher: National Aeronoautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1977
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 22
Subjects: Turbines.
Notes: Issued Dec. 1977.

Includes bibliographical references.