Single theory of continuous flow propulsions. Supersonic air-jet engines formula of thrust and flying (thrust) efficiency calculation
DOI:
https://doi.org/10.15587/2313-8416.2016.67086Keywords:
paraboloid zone of stagnant flow, kinematic analysis, theory of air-jet enginesAbstract
In the modern theory of air-jet engines (AJE) while formula of thrust and flying (thrust) efficiency calculation in zone H-d of the control contour while did not taken into care paraboloid zone of stagnant flow generation, as a physical phenomenon, that leaded to mistake calculation modern theory of the air-jet engines fundamental foundations such as: thermodynamic cycle of turbojet engine in coordinate P-V, T-S, formula of thrust and flying (thrust) efficiency, blowing profile rising force theorem, wrong using Euler’s equation. All this leaded to main physical processes wrong description while air-jet engine’s working process
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Copyright (c) 2016 Борис Шамшадович Мамедов, Ольга Валерьевна Лютова, Светлана Анатольевна Бовкун, Марианна Васильевна Скоробагатая, Елена Борисовна Корниенко, Дмитрий Иванович Харченко
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