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01178nam a2200241 a 4500 |
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20171111231150.0 |
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060727s1982 gr r f000 0 eng d |
040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
100 |
1 |
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|a Farrell, Charles A.
|
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
|
300 |
|
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|a 54 σ. :
|b εικ. ;
|c 28 εκ.
|
490 |
0 |
|
|a NASA technical paper
|v 2030
|
500 |
|
|
|a "Lewis Research Center."
|
504 |
|
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|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
|
952 |
|
|
|a GR-KoDPT
|b 59cc2c6c6c5ad13446fa62be
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|