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060921s1975 gr r f000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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| 100 |
1 |
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|a Penland, Jim A.
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| 245 |
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|a Aerodynamic characteristics of a hypersonic research airplane concept having a 70 swept double-delta wing at mach numbers from 1.50 to 2.86/
|c Jim A. Penland, Roger H. Fournier and Don C. Marcum ; Langley Research Center
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| 260 |
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|a Washington:
|b National Aeronautics and Space Administration,
|c 1975
|
| 300 |
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|a 81 σ. :
|b εικ. ;
|c 27 εκ.
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| 490 |
0 |
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|a NASA technical note
|v D-8065
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| 504 |
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|a Βιβλιογραφία: σ. 10-11
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| 650 |
|
0 |
|a Aerodynamics, Supersonic
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| 650 |
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0 |
|a Hypersonic planes
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| 650 |
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0 |
|a Delta wing airplanes
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| 650 |
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0 |
|a Research aircraft
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| 700 |
1 |
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|a Fournier, Roger H.
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| 700 |
1 |
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|a Marcum, Don C.
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| 710 |
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|a United States
|b National Aeronautics and Space Administration
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| 710 |
2 |
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|a Langley Research Center
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| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
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| 952 |
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|a GR-KoDPT
|b 59cc2d4c6c5ad13446fa78ff
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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