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스크램제트 재생냉각시스템의 복합열전달 해석을 위한 무격자 기법 해석자 개발
김재승(J.S. Kim),한다빈(D. Han),허진영(J.Y. Huh),김규홍(K.H. Kim) 한국전산유체공학회 2020 한국전산유체공학회지 Vol.25 No.4
A basic study was conducted to predict the internal thermal environment of an aircraft cruising at hypersonic speed. A numerical solver was developed using a meshless method to analyze the conjugate heat transfer of structures and cooling systems. Developed solver was validated comparing with a few analytic solutions for simple shapes. The solvers result was also verified with that from ABAQUS commercial solver for a 3-dimensional shape. In addition, Analysis of heat transfer including cooling channels confirmed that the heat capacity was preserved over time.