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01124nam a2200241 a 4500 |
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20171111231112.0 |
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090519s1978 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 Adamczyk, John J.
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| 245 |
1 |
0 |
|a Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory/
|c John J. Adamczyk
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1978
|
| 300 |
|
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|a 55 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 1345
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Flutter (Aerodynamics)
|
| 650 |
|
0 |
|a Ultrasonic waves
|x Speed
|
| 650 |
|
0 |
|a Disks, Rotating
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
| 710 |
2 |
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|a Lewis Research Center
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|
| 710 |
0 |
|
|b Scientific and Technical Information Office
|
| 952 |
|
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|a GR-KoDPT
|b 59cc25646c5ad13446f94a17
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
