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20171111230458.0 |
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070604s1983 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 Blair, A. B.
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| 245 |
1 |
0 |
|a Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers/
|c A.B. Blair, Jr., Jerry M. Allen, and Gloria Hernandez ; Langley Research Center
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| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1983
|
| 300 |
|
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|a 83 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
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|a NASA technical paper
|v 2157
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Guided missiles
|x Wings
|
| 650 |
|
0 |
|a Airplanes
|x Wings, Canard
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic
|
| 700 |
1 |
|
|a Allen, Jerry M.
|
| 700 |
1 |
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|a Hernandez, Gloria
|
| 710 |
|
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|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 |
|
|
|a GR-KoDPT
|b 59cc1f9f6c5ad13446f86225
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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