首页 | 本学科首页   官方微博 | 高级检索  
     检索      

改进跨音速位势方法的讨论
引用本文:朱自强,白雪松.改进跨音速位势方法的讨论[J].航空学报,1991,12(7):337-344.
作者姓名:朱自强  白雪松
作者单位:北京航空航天大学 (朱自强),北京航空航天大学(白雪松)
摘    要: 简要地回顾并讨论了传统位势方法之不足。对改进传统位势方法的两种必要的修正(熵修正和涡修正)的量级在小扰动条件下作了分析和估值。结果表明涡修正是更高阶小量,因而作为第一步修正可采用非等熵位势流来近似。采用熵修正激波算子来计及非等熵的激波突跃条件,并考虑了由熵修正带来的尾迹条件的变化。算例表明非等熵位势方法能得到预期的改进位势方法的效果。

关 键 词:跨音速流  位流  计算方法  

DISCUSSION OF IMPROVED TRANSONIC POTENTIAL METHOD
Beijing University of Aeronautics and Astronautics Zhu Ziqiang and Bai Xuesong.DISCUSSION OF IMPROVED TRANSONIC POTENTIAL METHOD[J].Acta Aeronautica et Astronautica Sinica,1991,12(7):337-344.
Authors:Beijing University of Aeronautics and Astronautics Zhu Ziqiang and Bai Xuesong
Institution:Beijing University of Aeronautics and Astronautics Zhu Ziqiang and Bai Xuesong
Abstract:In this paper some points concerning transonic potential method are briefly reviewed. The correction orders--nonisentropic jump condition and the vorticity generated behind the shock--are analysed and estimated then under the condition of small disturbance. Comparing two correction orders shows that vorticity correction is indeed of higher order. A nonisentropic potential formulation is described in this paper. Numerical examples depict that this nonisentropic method can simulate inviscid flow better than traditional potential method, while it has the advantage of simplicity in mathematical aspect as in original potential method.
Keywords:transonics  potential flow  calaulation methods  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号