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Pressurization of a Flightweight, Liquid Hydrogen Tank: Evaporation Condensation at the Liquid/Vapor Interface

机译:飞行重的液氢罐的加压:液/蒸气界面处的蒸发和冷凝

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This paper presents an analysis and simulation of evaporation and condensation at a motionless liquid/vapor interface. A 1-D model equation, emphasizing heat and mass transfer at the interface, is solved in two ways, and incorporated into a subgrid interface model within a CFD simulation. Simulation predictions are compared with experimental data from the CPST Engineering Design Unit tank, a cryogenic fluid management test tank in 1-g. The numerical challenge here is the physics of the liquid/vapor interface; pressurizing the ullage heats it by several degrees, and sets up an interfacial temperature gradient that transfers heat to the liquid phase—the rate limiting step of condensation is heat conducted through the liquid and vapor. This physics occurs in thin thermal layers O(1 mm) on either side of the interface which is resolved by the subgrid interface model. An accommodation coefficient of 1.0 is used in the simulations which is consistent with theory and measurements. This model is predictive of evaporation/condensation rates, that is, there is no parameter tuning.
机译:本文介绍了在不动的液/气界面处蒸发和冷凝的分析和模拟。一维模型方程式强调界面处的传热和传质,有两种解决方法,并将其纳入CFD模拟中的子网格界面模型中。将模拟预测结果与CPST工程设计单元储罐(1-g的低温流体管理测试储罐)中的实验数据进行比较。这里的数字挑战是液体/蒸汽界面的物理性质。对零头进行加压可将其加热数度,并建立一个将热量传递至液相的界面温度梯度-冷凝的限速步骤是通过液体和蒸气传导热量。这种物理现象发生在界面两侧的薄热层O(1 mm)中,这由子网格界面模型解决。模拟中使用的调节系数为1.0,这与理论和测量结果一致。该模型可预测蒸发/冷凝速率,即没有参数调整。

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