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钝化外形对旋成体气动性能的影响
引用本文:屈志朋,崔凯,胡守超,李广利.钝化外形对旋成体气动性能的影响[J].计算机辅助工程,2014,23(5):64-67.
作者姓名:屈志朋  崔凯  胡守超  李广利
作者单位:中国科学院力学研究所高温气体动力学国家重点实验室,北京,100190
基金项目:国家自然科学基金(90916013)
摘    要:为考察钝化外形对高超声速飞行器气动性能的影响,基于CFD分析,针对典型旋成体比较2种不同钝化外形(钝化半径均匀/非均匀)的气动性能.结果表明:在较小的钝化半径/高度下,由于前缘流向投影面积占整个旋成体流向投影面积比例较小,前缘气动性能对整个旋成体气动性能影响不大;但是,随着钝化半径/高度的增加,前缘气动性能对整个旋成体气动性能影响会逐渐增大.

关 键 词:旋成体  高超声速  飞行器  前缘  气动力  CFD
收稿时间:2013/6/14 0:00:00
修稿时间:2013/7/12 0:00:00

Effect of blunt shapes on aerodynamic performance of bodies of revolution
QU Zhipeng,CUI Kai,HU Shouchao and LI Guangli.Effect of blunt shapes on aerodynamic performance of bodies of revolution[J].Computer Aided Engineering,2014,23(5):64-67.
Authors:QU Zhipeng  CUI Kai  HU Shouchao and LI Guangli
Affiliation:State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences;State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences;State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences;State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences
Abstract:To study the effect of blunt shapes on the aerodynamic performance of hypersonic aircraft, based on CFD analysis, the aerodynamic performance of two different blunt shapes(the blunt radius are uniform or non uniform) are compared for typical bodies of revolution. The results show that, under the smaller blunt radius/height, because the projection area in flow direction of leading edge accounts for a small proportion of the projection area in flow direction of whole bodies of revolution, the leading edge aerodynamic performance has a little effect on the aerodynamic performance of the whole bodies of revolution; however, with the increase of blunt radius/height, the effect of leading edge aerodynamic performance on the aerodynamic performance of whole bodies of revolution increases gradually.
Keywords:body of revolution  hypersonic speed  aircraft  leading edge  aerodynamic force  CFD
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