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080902s1977 gr r 000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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1 |
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|a Sleeman, William C.
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|a Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee/
|c William C. Sleeman, Jr. and David R. Forsyth
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260 |
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|a Washington:
|b National Aeronautics and Space Administration,
|c 1977
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300 |
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|a 77 σ. :
|b εικ. ;
|c 27 εκ.
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490 |
0 |
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|a NASA technical note
|v 8488
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504 |
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|a Περιέχει βιβλιογραφικές παραπομπές
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650 |
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0 |
|a Lift (Aerodynamics)
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650 |
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0 |
|a Jet flaps (Airplanes)
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1 |
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|a Forsyth, David R.
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710 |
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|a United States
|b National Aeronautics and Space Administration
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710 |
0 |
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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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|a GR-KoDPT
|b 59cc2f496c5ad13446faaf69
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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