2 edition of Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade found in the catalog.
Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade
John F. Kline
by National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service in [Washington], Springfield, Va
Written in English
|Statement||JohnF. Kline, Roy G. Stabe, and Thomas P. Moffitt.|
|Series||NASA technical paper ; 1136, NASA technical paper -- 1136.|
|Contributions||Stabe, Roy G., Moffitt, Thomas P., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.|
|The Physical Object|
|Pagination||46 p. :|
|Number of Pages||46|
Use of English
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