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080610s1983 gr r f000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
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| 100 |
1 |
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|a Straight, David M.
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| 245 |
1 |
0 |
|a Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude/
|c David M. Straight and Richard R. Cullom
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| 260 |
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|a Washington:
|b National Aeronautics and Space Administration Scieentific and Technical Information Branch,
|c 1983
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| 300 |
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|a 36 σ. :
|b εικ. ;
|c 28 εκ.
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| 490 |
0 |
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|a NASA technical paper
|v 2171
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| 504 |
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Airplanes
|x Turbojet engines
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| 650 |
|
0 |
|a Airplanes
|x Flight testing
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| 650 |
|
0 |
|a Airplanes
|x Motors
|
| 700 |
1 |
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|a Cullom, Richard R.
|x Thrust
|
| 710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
| 710 |
2 |
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|a Lewis Research Center
|
| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|
| 710 |
0 |
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|b Scientific and Technical Information Branch
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| 952 |
|
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|a GR-KoDPT
|b 59cc2da46c5ad13446fa824c
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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