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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:
Turbines > Blades > Cooling
Turbines > Aerodynamics
Turbomachines > Performance
Table of Contents:
  • τ . 1. Performance with coolant ejection holes plugged
  • τ. 2. Performance with coolant flow ejection at temperature ratios up to 2

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