Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade
Title:
Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade
Author:
Kline, John F.
Personal Author:
Publication Information:
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978.
Physical Description:
46 pages : illustrations ; 27 cm.
General Note:
Issued Mar. 1978.
Language:
English
Format :
Book