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Time-averaged heat flux for a recessed tip, lip, and platform of a transonic turbine blade

Author(s):
Publication title:
A.S.M.E. paper
Title of ser.:
ASME Technical Paper : GT
Ser. no.:
2000
Pub. Year:
2000
No.:
2000-GT-197
Paper no.:
2000-GT-197
Pub. info.:
New York: American Society of Mechanical Engineers
Language:
English
Call no.:
A11800
Type:
Technical Paper

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