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Effects of film injection angle on turbine vane cooling

Effects of film injection angle on turbine vane cooling - - Washington, D.C. National Aeronautics and Space Administration 1977 - 23 p. - NASA TP 1095 : 1977 .

ISBN:

Subjects--Topical Terms:

Heat transfer, Film cooling, Turbine blades

Universal Decimal Class. No.: LNASA TP 1095 : 1977

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