2019
DOI: 10.1016/j.actaastro.2019.01.014
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Supersonic jet and nozzle flows in uniform-flow and free-vortex aerodynamic windows of gas lasers

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Cited by 10 publications
(7 citation statements)
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“…In cases where stationary energy supply is carried out in a supersonic flow (the energy supply intensity does not exceed a critical value), it is possible to design time-marching calculation schemes [16] (in a supersonic flow, the equations are hyperbolic in the x direction). To speed up the calculations, a vectorized approach to the fluxes calculation is used [17], which allows avoiding the programming of cyclic constructions.…”
Section: Methodsmentioning
confidence: 99%
“…In cases where stationary energy supply is carried out in a supersonic flow (the energy supply intensity does not exceed a critical value), it is possible to design time-marching calculation schemes [16] (in a supersonic flow, the equations are hyperbolic in the x direction). To speed up the calculations, a vectorized approach to the fluxes calculation is used [17], which allows avoiding the programming of cyclic constructions.…”
Section: Methodsmentioning
confidence: 99%
“…The width of the gas cavity is assumed equal to h = 5 mm. The intensity of energy supply is Q = 1 J/cm 3 .…”
Section: One-dimensional Modelmentioning
confidence: 99%
“…In a gas-discharge technological laser, the active element is a chamber filled with a working gas mixture. After the energy supply an excess amount of heat remains in the medium, which leads to increasing of the temperature and pressure of the gas mixture, as well as a change in the physical properties of the active medium [2,3]. Before initiating the next pulse, it is necessary to remove heat and to bring the medium to its initial thermodynamic state.…”
Section: Introductionmentioning
confidence: 99%
“…В газоразрядном технологическом лазере активный элемент представляет собой камеру, заполненную рабочей газовой смесью. После подвода энергии в среде остается избыточное количество тепла, которое приводит к увеличению температуры и давления газовой смеси, а также изменению физических свойств активной среды [2,3]. Перед инициированием следующего импульса необходимо осуществить отвод тепла и привести среду в исходное термодинамическое состояние.…”
Section: Introductionunclassified
“…Ширина газовой полости полагается равной h = 5 mm. Интенсивность подвода энергии составляет Q = 1 J/cm3 . Температура в щели в начальный момент принимает высокое значение, соответствующее величине подведенной энергии.…”
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