Prediction method for two-dimensional aerodynamic losses of cooled vanes using integral boundary-layer parameters
By: Louis J. Goldman and Raymond E. Gaugler
Contributors: Gaugler, Raymond E; Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper -- 1623
Publisher: U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 40
Subjects: Turbines -- Blades; Boundary layer; Aerodynamics
Notes: "Lewis Research Center."

"February 1980"--Cover

Subject category 02

Includes bibliographical references