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20171111231201.0 |
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080724s1976 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 Whitcomb, Richard T.
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| 245 |
1 |
0 |
|a A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets/
|c Richard T. Whitcomb
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration,
|c 1976
|
| 300 |
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|a [1], 30 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical note
|v 8260
|
| 504 |
|
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|a Βιβλιογραφία: σ. 15
|
| 650 |
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0 |
|a Airplanes
|x Wings
|
| 650 |
|
0 |
|a Drag (Aerodynamics)
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|
| 710 |
2 |
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|a Langley Research Center
|
| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
|
| 952 |
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|a GR-KoDPT
|b 59cc2e6e6c5ad13446fa97ab
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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