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大钝头短体跨音速大迎角不同流型的计算比较
引用本文:李津,朱自强,吴宗成,陈泽民. 大钝头短体跨音速大迎角不同流型的计算比较[J]. 航空学报, 2002, 23(4): 327-329
作者姓名:李津  朱自强  吴宗成  陈泽民
作者单位:北京航空航天大学,流体力学研究所,北京,100083;北京航空航天大学,流体力学研究所,北京,100083;北京航空航天大学,流体力学研究所,北京,100083;北京航空航天大学,流体力学研究所,北京,100083
基金项目:国家自然科学基金 (19882 0 0 1)资助项目
摘    要: 采用不同流型 (无粘,层流,湍流 )的数值模拟方法计算了绕大钝头短体外形的跨音速大迎角时的流态,并进行了比较分析。数值方法中选用 van Leer分裂格式离散无粘通量项,并构造了一种 Limiter函数以保证 TVD性质;采用中心差分格式来离散粘性通量项。湍流计算中采用了 B-L湍流模型。算例表明不同流型的流态共同特点是三维分离的非定常性,但不同流型计算所得流态的差异较大。

关 键 词:跨音速流  大钝头短体  大迎角分离流  非定常运动
文章编号:1000-6893(2002)04-0327-03
修稿时间:2001-09-17

COMPARISON OF COMPUTATIONAL RESULTS OF THE FLOW AROUND ABLUNT NOSED AND SHORT BODY AT LARGE ANGLES OF ATTACK
LI Jin,ZHU Zi qiang,WU Zong cheng,CHEN Ze min. COMPARISON OF COMPUTATIONAL RESULTS OF THE FLOW AROUND ABLUNT NOSED AND SHORT BODY AT LARGE ANGLES OF ATTACK[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(4): 327-329
Authors:LI Jin  ZHU Zi qiang  WU Zong cheng  CHEN Ze min
Affiliation:Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:The separated flow structures of the transonic flow around a blunt nosed and short body at large angles of attack are calculated by using three different types (inviscid, laminar and turbulent) of numerical simulations. Numerical results are compared with each other. In the numerical calculation van Leers Schemes is used to discretize the inviscid flux terms and a kind of limiter function is constructed to realize TVD character. The viscous flux terms are discretized by using a central difference scheme. B L model is used in the turbulent flow calculation. Numerical results show that the common feature of the 3 different separated flow structures is the unsteady quasi periodic character, while their detailed structures are quite different.
Keywords:transonic flow  a blunt nosed and short body  separated flow at a large angle of attack  unsteady flow
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