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01129nam a2200217 a 4500 |
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20171111231046.0 |
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050715s1980 gr r f000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
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|a Sanders, Bobby W.
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| 245 |
1 |
0 |
|a Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet/
|c Bobby W. Sanders
|
| 260 |
|
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|a Washington, D.C.:
|b NASA, Scientific and Technical Information Office,
|c 1980
|
| 300 |
|
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|a iii, 78 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 1532
|
| 500 |
|
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|a "Lewis Research Center."
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Airplanes
|x Turbojet engines
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|x Air intakes
|b Scientific and Technical Information Office
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office
|
| 710 |
2 |
|
|a Lewis Research Center
|
| 952 |
|
|
|a GR-KoDPT
|b 59cc216b6c5ad13446f8a6c6
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
