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01316nam a2200277 a 4500 |
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20171111231042.0 |
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081204s1985 gr r 000 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 Arbuckle, P. Douglas
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1 |
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|a Parametric study of a canard-configured transport using conceptual design optimization/
|c P. Douglas Arbuckle and Steven M. Sliwa
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260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1985
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300 |
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|a 25 σ. :
|b εικ. ;
|c 27 εκ.
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490 |
0 |
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|a NASA technical paper
|v 2400
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504 |
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|a Περιέχει βιβλιογραφικές παραπομπές (σ. 11-12)
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650 |
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0 |
|a Jet transports
|x Design and construction
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650 |
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0 |
|a Airplanes
|x Wings, Canard
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650 |
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0 |
|a Mathematical optimization
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650 |
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0 |
|a Aerodynamic configurations
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650 |
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0 |
|a Aircraft design
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650 |
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0 |
|a Canard configurations
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700 |
1 |
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|a Sliwa, Steven M.
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710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
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710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
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710 |
2 |
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|a Langley Research Center
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952 |
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|a GR-KoDPT
|b 59cc20d56c5ad13446f891fa
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|