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

Contributor(s): Language: English Series: NASA TP - 1603 : 1980Publication details: Washington, D.C. ; National Aeronautics and Space Administration ; 1980Edition: Description: 55 p; ISBN: Subject(s): | Computerized design, Aerodynamic configurations, Flow geometry, Profiles, Finite difference theoryOnline resources: Click here to access online
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Item type Current library Call number Status Date due Barcode Item holds
Pamphlets Standards Reports Pamphlets Standards Reports Central Library, IITB
LNASA TP - 1603 : 1980 Not for loan A41147
Total holds: 0

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