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.; Moffitt, Thomas P.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper ; 1136; 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.