Flow visualization of film cooling with spanwise injection from a small array of holes and compound-angle injection from a large array /
Louis M. Russell.

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Main Author: Russell, Louis M.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ;
Subjects: Flow visualization.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Cooling.
Turbines.
Note: Issued Apr. 1978.
Physical Description: 15 p. : ill. ; 27 cm.
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