높은 받음각에서 축대칭 물체의 공력 해석을 위한 회전/곡률 보정

초록

This paper present an enhanced computational analysis of tangent-ogive cylinder projectile at high angles of attack, incorporating a rotation/curvature(RC) correction to the k-ω SST RANS turbulence model. The empirical constants in Menter’s RC correction are optimized using Bayesian optimization to improve surface pressure predictions, particularly on the leeward side. These constants are trained on Lamont’s experimental data for a projectile with a nose fineness ratio of 3.5 at an angle of attack of 20° and a Reynolds number of 4.0×106 based on diameter. The improved correction is then validated on Tinling’s experimental data, which involves a slightly shorter nose with fineness ratio of 3.0, and shows better agreement with the measured surface pressure distribution.

출판유형
발행기관
한국전산유체학회지

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박진석
박진석
조교수

공기역학, 전산유체역학, 고성능 컴퓨팅을 연구하고 있습니다.