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|a GR-KoDPT
|b gre
|e AACR2
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1 |
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|a Pittman, James L.
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|a Body and canard effects on an attached-flow maneuver wing at Mach 1.62/
|c James L. Pittman and David S. Miller, William H. Mason
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| 260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1984
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| 300 |
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|a iii, 145 σ. :
|b εικ. ;
|c 28 εκ.
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| 490 |
0 |
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|a NASA technical paper
|v 2249
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| 504 |
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|a Περιέχει βιβλιογραφικές παραπομπές
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| 650 |
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0 |
|a Airplanes
|x Wings, Canard
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| 650 |
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0 |
|a Aerodynamics, Supersonic
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| 700 |
1 |
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|a Miller, David S.
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| 700 |
1 |
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|a Mason, William H.
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| 710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
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| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
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| 710 |
2 |
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|a Langley Research Center
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| 952 |
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|a GR-KoDPT
|b 59cc23026c5ad13446f8eb14
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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