空气动力学学报
空氣動力學學報
공기동역학학보
ACTA AERODYNAMICA SINICA
2009年
6期
723-728
,共6页
袁先旭%邓小兵%谢昱飞%张志成
袁先旭%鄧小兵%謝昱飛%張誌成
원선욱%산소병%사욱비%장지성
气动光学效应%RANS%LES%RANS/LES
氣動光學效應%RANS%LES%RANS/LES
기동광학효응%RANS%LES%RANS/LES
aero-optical effects%RANS%LES%RANS/LES
采用对接/拼接网格技术,建立了基于分区混合和基于湍流尺度混合的双重RANS/LES混合计算模型,并对环翼低速绕流、翼型跨声速绕流和球锥带凹窗外形二维超声速绕流进行了初步的数值模拟.环翼和翼型绕流计算表明,该混合模型可给出较合理的湍流宏观平均量;球锥带凹窗外形二维超声速绕流计算表明,该混合模型可得到超声速瞬态湍流脉动流场,凹窗处存在复杂的旋涡结构和波系结构,呈现较大尺度的脉动.但该模型还需要进一步的考核验证.
採用對接/拼接網格技術,建立瞭基于分區混閤和基于湍流呎度混閤的雙重RANS/LES混閤計算模型,併對環翼低速繞流、翼型跨聲速繞流和毬錐帶凹窗外形二維超聲速繞流進行瞭初步的數值模擬.環翼和翼型繞流計算錶明,該混閤模型可給齣較閤理的湍流宏觀平均量;毬錐帶凹窗外形二維超聲速繞流計算錶明,該混閤模型可得到超聲速瞬態湍流脈動流場,凹窗處存在複雜的鏇渦結構和波繫結構,呈現較大呎度的脈動.但該模型還需要進一步的攷覈驗證.
채용대접/병접망격기술,건립료기우분구혼합화기우단류척도혼합적쌍중RANS/LES혼합계산모형,병대배익저속요류、익형과성속요류화구추대요창외형이유초성속요류진행료초보적수치모의.배익화익형요류계산표명,해혼합모형가급출교합리적단류굉관평균량;구추대요창외형이유초성속요류계산표명,해혼합모형가득도초성속순태단류맥동류장,요창처존재복잡적선와결구화파계결구,정현교대척도적맥동.단해모형환수요진일보적고핵험증.
In this paper, a new double hybrid RANS/LES method is development for supersonic and hypersonic turbulence flows in order to research aero-optical effects. First, the computational zone is divided to RANS zone and RANS/LES zone, this is a zonal hybrid method based on patched grid technology. Secondly, in RANS/LES zone, a new hybrid model based BL turbulence inner model and Smagorinsky LES model is development. It belongs to DES method by Spalart, and is similar to Smagorinsky-Lilly model. Then the new method is used to compute several examples such as airfoil transonic turbulence flow, the results show that it can get reasonable turbulence average parameters. At last, a 2D sphere-cone with optical window model is computed by the new method, the supersonic and hypersonic turbulence fluctuation flow-fields is getting. It shows that there are complex vortex structures and wave structures and their interactions over the window, induced density fluctuation with high amplitude. But the new double hybrid RANS/LES method should be validated carefully.