Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row/

Main Author: Farrell, Charles A.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, Lewis Research Center, United States. National Aeronautics and Space Administration., Scientific and Technical Information Branch
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982
Series:NASA technical paper 2030
Subjects:
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245 1 0 |a Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row/  |c Charles A. Farrell 
260 |a Washington, D.C.:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1982 
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490 0 |a NASA technical paper  |v 2030 
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504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Aerodynamics, Transonic 
650 0 |a Impellers  |x Dynamics 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Branch 
710 2 |a Lewis Research Center 
710 0 |a United States.  |b National Aeronautics and Space Administration. 
710 0 |b Scientific and Technical Information Branch 
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