Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade /

Bibliographic Details
Main Author: Kline, John F
Corporate Author: United States National Aeronautics and Space Administration. Scientific and Technical Information Office
Other Authors: Moffitt, Thomas P, Stabe, Roy G
Format: Government Document Book
Language:English
Published: [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; for sale by the National Technical Information Service, 1978
Series:NASA technical paper 1136
Subjects:

Internet

Stanford University

Holdings details from Stanford University
Call Number: NAS 1.60:1136