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"In true rocket nozzles, the exhaust velocity is probably not uniform above the complete exit cross section and these velocity profiles are tough to evaluate correctly. A uniform axial velocity, ve, is assumed for all calculations which use just one-dimensional dilemma descriptions. This powerful exhaust velocity represents an average or https://raymondrhufr.activoblog.com/35290111/a-simple-key-for-ispaceplus-unveiled

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