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| 001 |
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20171111231156.0 |
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080619s1981 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 Calloway, Robert L.
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| 245 |
1 |
0 |
|a Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6/
|c Robert L. Calloway
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1981
|
| 300 |
|
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|a 23 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
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|a NASA technical paper
|v 1952
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Reusable space vehicles
|x Testing
|
| 650 |
|
0 |
|a Boundary layer
|x Testing
|
| 650 |
|
0 |
|a Wind tunnels
|x Testing
|
| 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 59cc2d746c5ad13446fa7d16
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
