空气动力学学报
空氣動力學學報
공기동역학학보
ACTA AERODYNAMICA SINICA
2014年
4期
481-487
,共7页
施永强%杨青真%黄秀全%郭霄
施永彊%楊青真%黃秀全%郭霄
시영강%양청진%황수전%곽소
振荡叶栅%谐波平衡方法%非定常流%双时间法%形状修正法
振盪葉柵%諧波平衡方法%非定常流%雙時間法%形狀脩正法
진탕협책%해파평형방법%비정상류%쌍시간법%형상수정법
oscillating cascade%harmonic balance method%unsteady flow%dual-time stepping method%shape correction method
为了提高叶轮机内周期性非定常流数值计算效率,发展了一种计算振荡叶栅非线性非定常流的谐波平衡方法,将周期性非定常流动参数采用傅里叶级数表示,从而将传统的定常流动数值计算方法应用于非定常流问题求解中,大大提高了非定常流计算效率。计算结果表明,发展的谐波平衡方法与线性方法、非线性时域法计算结果吻合较好,且其计算效率比时域法高1个数量级。另外,系统研究了谐波阶次对计算效率与计算精度的影响,认为在气流未出现严重分离时,应采用低阶谐波平衡方法,以减少计算耗时。此外,从压气机振荡叶栅非定常流场计算结果可以看出,叶片吸力面诱导涡的生成频率与振荡频率并不一致,涡生成频率要高于振荡频率。
為瞭提高葉輪機內週期性非定常流數值計算效率,髮展瞭一種計算振盪葉柵非線性非定常流的諧波平衡方法,將週期性非定常流動參數採用傅裏葉級數錶示,從而將傳統的定常流動數值計算方法應用于非定常流問題求解中,大大提高瞭非定常流計算效率。計算結果錶明,髮展的諧波平衡方法與線性方法、非線性時域法計算結果吻閤較好,且其計算效率比時域法高1箇數量級。另外,繫統研究瞭諧波階次對計算效率與計算精度的影響,認為在氣流未齣現嚴重分離時,應採用低階諧波平衡方法,以減少計算耗時。此外,從壓氣機振盪葉柵非定常流場計算結果可以看齣,葉片吸力麵誘導渦的生成頻率與振盪頻率併不一緻,渦生成頻率要高于振盪頻率。
위료제고협륜궤내주기성비정상류수치계산효솔,발전료일충계산진탕협책비선성비정상류적해파평형방법,장주기성비정상류동삼수채용부리협급수표시,종이장전통적정상류동수치계산방법응용우비정상류문제구해중,대대제고료비정상류계산효솔。계산결과표명,발전적해파평형방법여선성방법、비선성시역법계산결과문합교호,차기계산효솔비시역법고1개수량급。령외,계통연구료해파계차대계산효솔여계산정도적영향,인위재기류미출현엄중분리시,응채용저계해파평형방법,이감소계산모시。차외,종압기궤진탕협책비정상류장계산결과가이간출,협편흡력면유도와적생성빈솔여진탕빈솔병불일치,와생성빈솔요고우진탕빈솔。
A harmonic balance method for the analysis of nonlinear unsteady flow around oscillating cas-cades is developed to improve computational efficiency for the simulation of periodic flow in turbomachinery. The periodic unsteady flow parameters can be represented by a Fourier series.In this way,the unsteady problem can be solved using conventional computational fluid dynamic method for steady problem.The anal-ysis exploits the fact that,calculated results by harmonic balance are in good agreement with those from du-al-time stepping method and linear method,and present method is highly efficient;it is about one order of magnitude faster than conventional dual-time stepping method in the present computation.The effects of the number of harmonics are also studied.It shows that lower order harmonic balance methods are sufficient to simulate periodic unsteady flow accurately except the flow fields including serious separated domain.So, lower order harmonic balance methods could be adopted to analysis unsteady flow in turbomachinery to re-duce the computational cost.In addition,the characteristic of unsteady flow around a compressor cascade is investigated,and the mechanism of generation of separated vortex and the vortex shedding frequency are also analyzed.