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|a GR-KoDPT
|b gre
|e AACR2
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1 |
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|a Frassinelli, Mark C.
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|a Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles/
|c Mark C. Frassinelli, George T. Carson, Jr
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260 |
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|a Washington:
|b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
|c 1990
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300 |
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|a 56 σ. :
|b εικ. ;
|c 28 εκ.
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490 |
0 |
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|a NASA technical paper
|v 3036
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504 |
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|a Βιβλιογραφία: σ. 11
|
650 |
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0 |
|a Airplanes
|x Tail surfaces
|
650 |
|
0 |
|a Stability of airplanes, Longitudinal
|
650 |
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0 |
|a Aerodynamics, Transonic
|
650 |
|
0 |
|a Jet nozzles
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700 |
1 |
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|a Carson, George T.
|
710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Division
|
710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Division
|
710 |
2 |
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|a Langley Research Center
|
952 |
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|a GR-KoDPT
|b 59cc29996c5ad13446f9ed9d
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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