Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes
Subtitle: II-performance with coolant flow ejection at temperature ratios up to 2
By: Jeffrey E. Haas and Milton G. Kofskey
Contributors: Kofskey, Milton G , joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1057
Publisher: National Aeronautics 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: 31
Subjects: Aerodynamics; Airplanes -- Turborjet engines -- Cooling
Notes: Issued Oct. 1977

Includes bibliographical references