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20171111230457.0 |
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081205s1986 gr r 000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
|
|a Mann, Michael J.
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| 245 |
1 |
0 |
|a Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method/
|c Michael J. Mann and Charles E. Mercer
|
| 260 |
|
|
|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1986
|
| 300 |
|
|
|a 181 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 2628
|
| 650 |
|
0 |
|a Aerodynamics, Transonic
|
| 700 |
1 |
|
|a Mercer, Charles E.
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
|
| 710 |
2 |
|
|a Langley Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc1f826c5ad13446f85cad
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
