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| 008 |
081127s1980 gr r 000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
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|a Freeman, Carl E.
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| 245 |
1 |
0 |
|a Development and validation of a combined rotor-fuselage induced flow-field computational method/
|c Carl E. Freeman
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1980
|
| 300 |
|
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|a 58 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 1656
|a AVRADCOM technical report
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|v 80-B-3
|
| 650 |
|
0 |
|a Rotors (Helicopters)
|x Aerodynamics
|
| 650 |
|
0 |
|a Aerodynamics
|x Mathematical models
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office
|
| 710 |
2 |
|
|a Langley Research Center
|
| 710 |
0 |
|
|a Army Research and Technology Laboratories U.S.
|b Structures Laboratory
|
| 952 |
|
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|a GR-KoDPT
|b 59cc1e246c5ad13446f817f4
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
