Numerical Code Validations and Quantitative Analyses of Ice Accretion Shapes
Quantitativeanalyses of ice accretion shapes have not been sufficiently investigated in previous researches; consequently, there are limitations to judge the accuracy of numerical codes and to analyze the change of ice accretion shapes in various icing conditions. In this study, the developed code has been quantitatively validated with available experiments and the other numerical codes on the cylinder and the airfoil. Maximum thickness, its heading direction and ice accretion area are quantified and expressed in the polar coordinate system for the comparison with other numerical results of NASA, ONERA and DRA, The comparison among the present code and the other codes yields sufficiently accurate results for the analyses of ice accumulated shapes with various icing conditions. It was found that discrepancy of ice shapes around the cylinder turns out to be greater than those of the airfoil, which is due to the incapability of the present code to capture the massive separation. However, the present code yields the highly reliable and consistent results for the airfoil shapes.
aircraft icing polar coordinate system ice accretion shapes ice heading direction maximum thickness
Son Chankyu Oh Sejong Yee Kwanjung
Department of Aerospace Engineering ,Pusan National University, Busan, Korea
国际会议
2010 Asia-Pacific International Symposium on Aerospace Technology(2010 亚太航空航天技术研讨会 APISAT 2010)
西安
英文
345-349
2010-09-01（万方平台首次上网日期，不代表论文的发表时间）