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081204s1987 gr r 000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
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| 100 |
1 |
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|a Cunningham, Herbert J.
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| 245 |
1 |
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|a Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip missile and comparison with experiment and PANAIR/
|c Herbert J. Cunningham
|
| 260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1987
|
| 300 |
|
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|a 26 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical paper
|v 2736
|
| 650 |
|
0 |
|a Unsteady flow (Aerodynamics)
|x Computer simulation
|
| 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
|
| 710 |
2 |
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|a Langley Research Center
|
| 952 |
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|a GR-KoDPT
|b 59cc20576c5ad13446f88059
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
