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Cold-air experimental investigation of a turbine with blade trailing-edge coolant ejection I-single-stage turbine

Cold-air experimental investigation of a turbine with blade trailing-edge coolant ejection I-single-stage turbine - - Washington, D.C. NASA 1975 - 39 p. - NASA TM X 3214 : 1975 .

ISBN:

Subjects--Topical Terms:

Turbine, Turbine aerodynamics, Turbine performance, Blade cooling

Universal Decimal Class. No.: LNASA TM X 3214 : 1975

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