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Film-Cooling Effectiveness from Shaped Film Cooling Holes for a Gas Turbine Blade.

Author(s):
Publication title:
A.S.M.E. paper
Title of ser.:
ASME Technical Paper : GT
Ser. no.:
2008
Pub. Year:
2008
No.:
GT2008-50916
Paper no.:
GT2008-50916
Pages:
12
Pub. info.:
New York, NY: American Society of Mechanical Engineers
Language:
English
Call no.:
A11800
Type:
Technical Paper

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