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Investigation of the Influence of Trailing Edge Shock Waves on the Film Cooling Performance of Gas Turbine Airfoils.

Author(s):
Publication title:
A.S.M.E. paper
Title of ser.:
ASME Technical Paper : GT
Ser. no.:
2007
Pub. Year:
2007
No.:
GT2007-27482
Paper no.:
GT2007-27482
Pages:
10
Pub. info.:
New York, NY: American Society of Mechanical Engineers
Language:
English
Call no.:
A11800
Type:
Technical Paper

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