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050519s1976 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 Crawford, Davis H.
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| 245 |
1 |
0 |
|a Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3/
|c Davis H. Crawford
|
| 260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration ,
|c 1976
|
| 300 |
|
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|a 48 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical note
|v NASA TN D-8203
|
| 500 |
|
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|a "Lanlgley Research Center"--σ.τ.
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Heat
|x Transmission
|
| 650 |
|
0 |
|a Space vehicles
|
| 650 |
|
0 |
|a Aerothermodynamics
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration
|
| 710 |
2 |
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|a Langley Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc231d6c5ad13446f8efb6
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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