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050714s1980 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 Quinn, Robert D.
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| 245 |
1 |
0 |
|a In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0/
|c Robert D. Quinn and Leslie Gong
|
| 260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1980
|
| 300 |
|
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|a 49 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical paper
|v 1764
|
| 500 |
|
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|a "Dryden Flight Research Center."
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
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0 |
|a Turbulent boundary layer
|
| 650 |
|
0 |
|a Heat
|x Transmission
|
| 700 |
1 |
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|a Gong, Leslie
|
| 710 |
|
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|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 |
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|a Hugh L. Dryden Flight Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc213b6c5ad13446f8a076
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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