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computational simulation of shock-bubble interaction, using a front-tracking/ghost fluid method
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نویسنده
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razmi a. ,taeibi-rahni m. ,massah h. r. ,terashima h. ,moezzi h.
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منبع
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journal of applied fluid mechanics - 2019 - دوره : 12 - شماره : 2 - صفحه:631 -645
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چکیده
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A front tracking/ghost fluid method was used to simulate fluid interfaces in a shock–bubble interaction problem. the method captures fluid interfaces, using explicit front-tracking and defines interface conditions, using the ghost-fluid method. in order to demonstrate the accuracy and the capability tracking of the approach used, an airhelium and anair-r22 shock-bubble interaction cases were simulated. the computational results were compared with reliable experimental and computational studies, showing close agreements.
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کلیدواژه
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computational simulation; front tracking/ghost fluid method; shock-bubble interaction; supersonic flow
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آدرس
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sharif university, department of aerospace engineering, iran, sharif university, department of aerospace engineering, iran. aerospace research institute, iran, acoustical engineering society of iran, iran, hokkaido university, faculty of engineering, japan, sharif university, department of aerospace engineering, iran
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پست الکترونیکی
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moezzi.ae@gmail.com
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Authors
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