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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 Johnson, William G.
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| 245 |
1 |
0 |
|a Aerodynamic characteristics of a powered, externally blown flap STOL transport model with two engine simulator sizes/
|c William G. Johnson ; 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 291 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical note
|v D-8057
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| 504 |
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|a Βιβλιογραφία: σ. 16
|
| 650 |
|
0 |
|a Flaps (Airplanes)
|
| 650 |
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0 |
|a Short take-off and landing aircraft
|
| 650 |
|
0 |
|a Aerodynamic measurements
|
| 710 |
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|a United States
|b National Aeronautics and Space Administration
|
| 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 59cc2d556c5ad13446fa79e4
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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