Joule-Thomson effect and flow behavior for energy-efficient dehydration of high-pressure natural gas in supersonic separator

Wang, Shiwei; Wang, Chao; Ding, Hongbing; Zhang, Yu; Dong, Yuanyuan; Wen, Chuang

doi:10.1016/j.energy.2023.128122

Cited by 6 publications

(1 citation statement)

References 49 publications

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“…Research Object Research Approach [17] cell culture EWF model [19] Gas-liquid Cylindrical Cyclones [20] Containment cooling system [21] Containment condenser [22] Atmospheric pressure tower [15] Supersonic Separator Eulerian-Lagrangian and EWF model [23] Ultrasound separator [18] Baffle mist eliminator Discrete Phase model and EWF model [24] Football field wind-driven rain [25] Surface of nuclear power plant containment vessel Species Transport Model and EWF model [26] Natural gas station pipeline Mixture model and EWF model…”

Section: Referencementioning

confidence: 99%

Numerical Investigation of the Water-Drop Impact on Low-Drag Airfoil Using the Euler–Euler Approach and Eulerian Wall Film Model

et al. 2023

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The Eulerian Wall Film (EWF) model is a mathematical model employed to analyze the behavior of fluid films on a surface. The model has been widely adopted in various engineering applications due to its accuracy and efficiency. However, it is rarely applied in the aerospace field. The solution of the water-drop impact constitutes an indispensable prerequisite for the computation of ice accretion on the exterior of aircraft wings. In this study, we propose a novel approach for the estimation of water-drop impact on wing surfaces by integrating the Euler–Euler approach and EWF model. This approach is capable of furnishing a point of reference and a theoretical foundation for prospective water-drop impact experiments. Through comparison with pertinent experimental findings, the precision of the numerical simulation approach utilized in this paper is substantiated. Specifically, the research object is the NACA653-218 airfoil of the C-919 transport aircraft, for which the aerodynamic properties, water-drop collision, and liquid film flow characteristics during steady flight were simulated.

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