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
Published
1978
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
Edition Notes
| Statement | JohnF. Kline, Roy G. Stabe, and Thomas P. Moffitt |
| Series | NASA technical paper ; 1136 |
| Contributions | Stabe, Roy G., joint author, Moffitt, Thomas P., joint author, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office |
| The Physical Object | |
|---|---|
| Pagination | 46 p. : |
| Number of Pages | 46 |
| ID Numbers | |
| Open Library | OL14931937M |
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