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081205s1986 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 Ruhlin, Charles L.
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| 245 |
1 |
0 |
|a Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model/
|c Charles L. Ruhlin, Kumar G. Bhatia, and K.S. Nagaraja
|
| 260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1986
|
| 300 |
|
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|a 73 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical paper
|v 2627
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| 650 |
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0 |
|a Flutter (Aerodynamics)
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| 650 |
|
0 |
|a Aeroelasticity
|
| 650 |
|
0 |
|a Structural engineering
|z United States
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| 700 |
1 |
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|a Bhatia, Kumar G.
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| 700 |
1 |
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|a Nagaraja, K. S.
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
|
| 710 |
2 |
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|a Langley Research Center
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| 952 |
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|a GR-KoDPT
|b 59cc1f416c5ad13446f84fd6
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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