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NUMERICAL MODELING OF FLUID TRANSIENTS BY A FINITE VOLUME PROCEDURE FOR ROCKET PROPULSION SYSTEMS

机译:火箭推进系统有限体积过程流体瞬变的数值模拟

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This paper describes the application of a finite volume procedure for a fluid network to predict fluid transients following a rapid valve closure in a long cryogenic pipeline. The conservation equations of mass, momentum, energy, and the equation of state for real fluids are solved in the fluid network consisting of nodes and branches. In the present formulation, the speed of sound does not appear explicitly in the governing equations. Instead, the equation of state for a real fluid is solved in conjunction with the conservation equations to calculate the compressibility factor for modeling the wave propagation phenomenon. The numerical procedure is also capable of modeling the wave propagation due to phase change and gas-liquid mixture. The predicted history of pressure and velocity variation in a single pipe has been compared to the solution by the method of characteristics (MOC) for liquid oxygen (LO_2), liquid hydrogen (LH_2), and water (H_2O). The paper also presents the numerical solution of pressure surges for a gas-liquid mixture, condensation of vapor, and flow circuit with parallel branches and tailpipe.
机译:本文介绍了用于流体网络的有限体积过程的应用,以在长低温管道中快速阀闭合后预测流体瞬变。在由节点和分支组成的流体网络中解决了质量,动量,能量和状态的状态等方程的保护方程。在本制定中,在控制方程中没有明确出现声音的速度。相反,真实流体状态的等式结合保护方程来解决以计算用于建模波传播现象的可压缩因子。数值过程还能够通过相变和气液混合物来建模波传播。通过用于液氧(LO_2),液态氢(LH_2)和水(H_2O)的特性(MOC)的方法,将单管中的压力和速度变化的预测历史与溶液进行比较。本文还介绍了气液混合物,蒸汽冷凝和具有平行分支和尾管的流动回路的压力浪涌的数值溶液。

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