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Computer program for generating input for analysis of impingement cooled, axial-flow turbine blade

Computer program for generating input for analysis of impingement cooled, axial-flow turbine blade - - Washington, D.C. National Aeronautics and Space Administration 1980 - 55 p. - NASA TP - 1603 : 1980 .

ISBN:

Subjects--Topical Terms:

Computerized design, Aerodynamic configurations, Flow geometry, Profiles, Finite difference theory

Universal Decimal Class. No.: LNASA TP - 1603 : 1980

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