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20171111230456.0 |
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081203s1985 gr r 000 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 Avery, Don E.
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| 245 |
1 |
0 |
|a Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7/
|c Don E. Avery
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1985
|
| 300 |
|
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|a 47 σ. :
|b έγχρ. εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical paper
|v 2307
|
| 650 |
|
0 |
|a Cold surfaces
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| 650 |
|
0 |
|a Heat shielding
|
| 650 |
|
0 |
|a Hypersonic flow
|
| 650 |
|
0 |
|a Impingement
|
| 650 |
|
0 |
|a Reusable heat shielding
|
| 650 |
|
0 |
|a Thermal protection
|
| 650 |
|
0 |
|a Tiles
|
| 650 |
|
0 |
|a Turbulent boundary layer
|
| 650 |
|
0 |
|a Turbulent flow
|
| 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
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| 952 |
|
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|a GR-KoDPT
|b 59cc1f5d6c5ad13446f85538
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
