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20171111231204.0 |
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050302s1976 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 Hawkins, J. E.
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| 245 |
1 |
0 |
|a Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry, supersonic inlet configuration/
|c J.E. Hawkins, F.P. Kirkland, and R.L. Turner
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| 260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration,
|c 1976
|
| 300 |
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|a 106 σ., 3 διπλωμένα φύλλα με πίνακες :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
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|a NASA contractor report
|v NASA CR-2680
|
| 500 |
|
|
|a "Prepared by General Dynamics' Convair Aerospace Division for Ames Research Center"
|
| 504 |
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Jet engines
|x Air intakes
|
| 700 |
1 |
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|a Kirkland, F. P.
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| 700 |
1 |
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|a Turner, R. L.
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|
| 710 |
2 |
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|a General Dynamics' Convair Aerospace Division
|
| 710 |
0 |
|
|a Ames Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc2ecd6c5ad13446faa1ec
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
