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01093nam a2200229 a 4500 |
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20171111230503.0 |
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081203s1984 gr r 000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
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|a Yaros, Steven F.
|
| 245 |
1 |
0 |
|a Theoretical and experimental engine-inlet flow fields for fighter forebodies/
|c Steven F. Yaros
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1984
|
| 300 |
|
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|a 63 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 2270
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Fighter planes
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic
|
| 650 |
|
0 |
|a Aerodynamics, Transonic
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
|
| 710 |
2 |
|
|a Langley Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc20306c5ad13446f879da
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
