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|a GR-KoDPT
|b gre
|e AACR2
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|a Stallings, Robert L.
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|a Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds/
|c Robert L. Stallings, Jr., Milton Lamb, and Carolyn B. Watson
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| 260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1980
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| 300 |
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|a [108] σ. :
|b εικ. ;
|c 27 εκ.
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| 490 |
0 |
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|a NASA technical paper
|v 1683
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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
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| 650 |
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0 |
|a Stability of airplanes
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| 700 |
1 |
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|a Lamb, Milton
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| 700 |
1 |
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|a Watson, Carolyn B.
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| 710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
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| 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
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| 952 |
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|a GR-KoDPT
|b 59cc257c6c5ad13446f94db7
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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