Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade
By: JohnF. Kline, Roy G. Stabe, and Thomas P. Moffitt
Contributors: Stabe, Roy G., joint author; Moffitt, Thomas P., joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1136
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 46
Subjects: Turbines -- Aerodynamics; Turbines -- Blades -- Cooling
Notes: Issued Mar. 1978

Includes bibliographical references