MODELING OF GAS-DYNAMIC PROCESSES IN THE ELEMENTS OF IMPULSE EJECTOR

G. Voropaiev, I. Zagumennyi, N. Rozumnyuk
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引用次数: 1

Abstract

The paper presents the numerical results on gas-dynamic processes in various elements of the impulse ejector, including pre-chamber, supersonic nozzle and mixing chamber, to determine optimal geometric parameters providing the given flow rate characteristics. At an extra-high pressure of the ejecting gas (>100 bar) it is impossible to create a nozzle design with continuously changing cross-sectional area and limited nozzle length. So, it is necessary to place a pre-chamber between the gas generator and the ejector nozzle for throttling full gas pressure. In order to optimize the pre-chamber parameters in the ejector with discrete holes of the gas generator and the operating pressure in the range of 400÷1000 bar, a series of calculations were performed to determine the pre-chamber parameters, ensuring stable operation of the supersonic annular nozzle at the high pressure of 35÷45 bar and the flow rate of 0.5÷0.6 kg/s. 3D numerical simulation of the gas flow into the pre-chamber through the gas generator holes shows the degree of the flow pattern non-uniformity in the pre-chamber at the ejector nozzle inlet is quite low. This justifies the numerical simulation of gas flow in the ejector in axisymmetric formulation and allows restricting the number of the gas generator holes without inducing significant non-uniformity in the azimuthal direction.
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脉冲喷射器元件中气体动力学过程的建模
本文给出了脉冲喷射器各部件(包括预室、超声速喷管和混合室)内气体动力学过程的数值结果,以确定在给定流量特性下的最优几何参数。在超高压喷射气体(>100 bar)下,不可能设计出横截面积不断变化且喷嘴长度有限的喷嘴。因此,有必要在燃气发生器和喷射器喷嘴之间放置预室,以节流全气压力。为了优化气体发生器离散孔喷射器预室参数和工作压力在400÷1000 bar范围内,通过一系列计算确定了预室参数,确保超声速环形喷管在高压35÷45 bar和流量0.5÷0.6 kg/s下稳定工作。通过气体发生器孔进入预室的三维数值模拟表明,喷射器入口处预室内流型不均匀程度很低。这证明了以轴对称形式对喷射器内气体流动的数值模拟是正确的,并且可以在不引起方位角明显不均匀的情况下限制气体发生器孔的数量。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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