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|a GR-KoDPT
|b gre
|e AACR2
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| 100 |
1 |
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|a Powers, Sheryll Goecke
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| 245 |
1 |
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|a Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers/
|c Sheryll Goecke Powers, Jarrett K. Huffman and Charles H. Fox, Jr
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| 260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1986
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| 300 |
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|a 139 σ. :
|b εικ. ;
|c 27 εκ.
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| 490 |
0 |
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|a NASA technical paper
|v 2638
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| 650 |
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0 |
|a Mach number
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| 650 |
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0 |
|a Drag (Aerodynamics)
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| 700 |
1 |
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|a Huffman, Jarrett K.
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| 700 |
1 |
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|a Fox, Charles H.
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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 Dryden Flight Research Center
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| 952 |
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|a GR-KoDPT
|b 59cc1f726c5ad13446f85992
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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