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050126s1982 gr r f000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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100 |
1 |
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|a Moretti, Gino
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245 |
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|a Calculation of three-dimensional, inviscid supersonic, steady flows/
|c Gino Moretti ; prepared for Langley Research Center under grant NSG-1248
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260 |
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|a Washington, D.C.:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1982
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300 |
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|a iii, 118 σ. :
|b εικ. ;
|c 28 εκ.
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490 |
0 |
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|a NASA contractor report
|v NASA CR-3573
|
500 |
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|a "Polytechnic Institute of New York."
|
504 |
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|a Περιέχει βιβλιογραφικές παραπομπές
|
650 |
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0 |
|a Aerodynamics, Supersonic
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650 |
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0 |
|a Airplanes
|x Fuselage
|
650 |
|
0 |
|a Airframes
|
710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office
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710 |
2 |
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|a Langley Research Center
|
710 |
2 |
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|a Polytechnic Institute of New York
|
952 |
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|a GR-KoDPT
|b 59cc2dfd6c5ad13446fa8b75
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|