Approximate Analytical Method of Computation of Optimal Rocket Engine Supersonic Nozzle Contour.

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作者：
Kevo, Milko [1 ]
机构：
[1] OOUR Inzenjering, INA-Projekt,, Zagreb, Yugosl, OOUR Inzenjering, INA-Projekt, Zagreb, Yugosl
来源：
| 1600年 / 27期
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摘要：
ROCKET ENGINES
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