空气动力学学报
空氣動力學學報
공기동역학학보
ACTA AERODYNAMICA SINICA
2014年
5期
694-699
,共6页
张扬%白俊强%华俊%徐晶磊
張颺%白俊彊%華俊%徐晶磊
장양%백준강%화준%서정뢰
湍流模型%剪切应力%雷诺方程%混合 RANS/LES 方法
湍流模型%剪切應力%雷諾方程%混閤 RANS/LES 方法
단류모형%전절응력%뢰낙방정%혼합 RANS/LES 방법
turbulence model%shear stress%Reynolds equation%hybrid RANS/LES method
为了提高涡粘性假设的湍流模型对于非稳态流动的求解精度,同时兼顾其对于稳态流动的求解性能,将雷诺应力项与连续变换方程(CSSE)结合而形成新的应力项,使其根据流场尺度、网格尺度及 Kolmogorov 尺度来自动调节当地的应力雷诺应力模化水平,避免网格因素在流场模拟中产生不利影响,改正了混合 RANS/LES 方法的速度型偏离对数率问题;同时,该方法并未引入显式亚格子模型(SGS),因此回避了亚格子系数确定对于流场模拟精度产生的影响,改善了湍流模型对于流动不稳定性的辨识精度。在湍流平板算例中,CSSE 方法计算的边界层速度型精度与雷诺平均方法(RANS)相当,而对于圆柱尾迹的模拟则证明了 CSSE 方法具有混合 RANS/LES 方法的优点,即能够准确模拟流动的不稳定性特征。
為瞭提高渦粘性假設的湍流模型對于非穩態流動的求解精度,同時兼顧其對于穩態流動的求解性能,將雷諾應力項與連續變換方程(CSSE)結閤而形成新的應力項,使其根據流場呎度、網格呎度及 Kolmogorov 呎度來自動調節噹地的應力雷諾應力模化水平,避免網格因素在流場模擬中產生不利影響,改正瞭混閤 RANS/LES 方法的速度型偏離對數率問題;同時,該方法併未引入顯式亞格子模型(SGS),因此迴避瞭亞格子繫數確定對于流場模擬精度產生的影響,改善瞭湍流模型對于流動不穩定性的辨識精度。在湍流平闆算例中,CSSE 方法計算的邊界層速度型精度與雷諾平均方法(RANS)相噹,而對于圓柱尾跡的模擬則證明瞭 CSSE 方法具有混閤 RANS/LES 方法的優點,即能夠準確模擬流動的不穩定性特徵。
위료제고와점성가설적단류모형대우비은태류동적구해정도,동시겸고기대우은태류동적구해성능,장뢰낙응력항여련속변환방정(CSSE)결합이형성신적응력항,사기근거류장척도、망격척도급 Kolmogorov 척도래자동조절당지적응력뢰낙응력모화수평,피면망격인소재류장모의중산생불리영향,개정료혼합 RANS/LES 방법적속도형편리대수솔문제;동시,해방법병미인입현식아격자모형(SGS),인차회피료아격자계수학정대우류장모의정도산생적영향,개선료단류모형대우류동불은정성적변식정도。재단류평판산례중,CSSE 방법계산적변계층속도형정도여뢰낙평균방법(RANS)상당,이대우원주미적적모의칙증명료 CSSE 방법구유혼합 RANS/LES 방법적우점,즉능구준학모의류동적불은정성특정。
In order to get the higher precision of the unsteady flow predicted by using liner turbulence model as well as keep the capability of solving the steady flow,the Reynolds-stress term is combined with continuous scale switch equation(CSSE)to form one new stress term which can automatically adjust the local Reynolds-stress level according to the flow field scale,grid scale and Kolmogorov scale.The CSSE method eliminates the disadvantage of grid scale on the flow simulation,the problem of disagreement between the velocity profile obtained by the method of hybrid RANS/LES and the law of the wall is solved.Meanwhile, this method do not use the explicit sub-grid stress(SGS)model which can avoid the disadvantaged impact on the flow simulation caused by SGS coefficient,so the flow instability can be controlled more accurately .The simulations of the boundary flow of the plate and the flow over the cylinder both prove that CSSE method is robust.In the testcase of a turbulent flat-plate,the velocity profiles of flat-plate boundary layer solved by CSSE match with that solved by Reynolds averaged Navier-Stocks(RANS)method very closely,the simula-tion of cylinder wake proves that the CSSE method can precisely simulate the flow instability which is the ad-vantage of hybrid RANS/LES.