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

Main Author: Rosenbaum, David
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Propulsion Laboratory U.S., Army Research and Technology Laboratories U.S. Structures Laboratory, Lewis Research Center
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Series:NASA technical paper AVRADCOM technical report 1603
Subjects:
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245 1 0 |a Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade/  |c David Rosenbaum 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1980 
300 |a 53 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical paper  |v 1603  |a AVRADCOM technical report 
504 |a Περιέχει βιβλιογραφικές παραπομπές  |v 79-34 
650 0 |a Turbines  |x Blades 
650 0 |a Jets  |x Fluid dynamics  |x Data processing 
650 0 |a Heat  |x Transmission 
710 |a United States  |b National Aeronautics and Space Administration  |x Computer programs  |b Scientific and Technical Information Branch 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch 
710 2 |a Propulsion Laboratory U.S. 
710 0 |a Army Research and Technology Laboratories U.S.  |b Structures Laboratory 
710 2 |a Lewis Research Center 
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