Effect of coolant flow ejection on aerodynamic performance of low-aspect-ration vanes/

Main Author: Haas, Jeffrey E.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Office, Lewis Research Center, United States. National Aeronautics and Space Administration., Scientific and Technical Information Office
Other Authors: Kofskey, Milton G.
Format: Book
Language:English
Published: Washington: NASA Scientific and technical Information Branch, 1976-1977
Series:NASA technical paper 1057
Subjects:
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100 1 |a Haas, Jeffrey E. 
245 1 0 |a Effect of coolant flow ejection on aerodynamic performance of low-aspect-ration vanes/  |c Jeffrey E. Haas and Milton G. Kofskey 
260 |a Washington:  |b NASA Scientific and technical Information Branch,  |c 1976-1977 
300 |a 2 τ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA technical paper  |v 1057 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
505 0 |a τ . 1. Performance with coolant ejection holes plugged -- τ. 2. Performance with coolant flow ejection at temperature ratios up to 2 
650 0 |a Turbines  |x Blades  |x Cooling 
650 0 |a Turbines  |x Aerodynamics 
650 0 |a Turbomachines  |x Performance 
700 1 |a Kofskey, Milton G. 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Office 
710 2 |a Lewis Research Center 
710 0 |a United States.  |b National Aeronautics and Space Administration. 
710 0 |b Scientific and Technical Information Office 
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