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080520s1975 gr r f000 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 Maiden, Donald L.
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| 245 |
1 |
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|a Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to mach 2.01/
|c Donald L. Maiden
|
| 260 |
|
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|a Washington:
|b NASA,
|c 1975
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| 300 |
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|a 75 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
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|a NASA technical note
|v 7906
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| 504 |
|
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|a Βιβλιογραφία: σ. 17
|
| 650 |
|
0 |
|a Jet nozzles
|x Testing
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|
| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
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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 59cc2c076c5ad13446fa53e9
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
