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080602s1976 gr r 000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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100 |
1 |
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|a Iliff, Kenneth W.
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245 |
1 |
0 |
|a Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8-scale F-15 airplane model obtained from flight tests/
|c Kenneth W. Iliff, Richard E. Maine and Mary F. Shafer
|
260 |
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|a Washington:
|b NASA,
|c 1976
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300 |
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|a 31 σ. :
|b εικ. ;
|c 28 εκ.
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490 |
0 |
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|a NASA technical note
|v 8136
|
504 |
|
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|a Βιβλιογραφία: σ. 13
|
650 |
|
0 |
|a Eagle (Jet fighter plane)
|x Models
|x Testing
|
650 |
|
0 |
|a Stability of airplanes
|
650 |
|
0 |
|a Airplanes
|x Control systems
|
700 |
1 |
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|a Maine, Richard E.
|
700 |
1 |
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|a Shafer, Mary F.
|
710 |
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|a United States
|b National Aeronautics and Space Administration
|
710 |
2 |
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|a Flight Research Center
|
710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
|
952 |
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|a GR-KoDPT
|b 59cc2d966c5ad13446fa80c2
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|