机械工程学报
機械工程學報
궤계공정학보
CHINESE JOURNAL OF MECHANICAL ENGINEERING
2014年
22期
186-191
,共6页
刘栋%朱鹣%朱方能%杨晓勇%金亨凡
劉棟%硃鶼%硃方能%楊曉勇%金亨凡
류동%주겸%주방능%양효용%금형범
泰勒涡动%粒子图像测速技术(Particle image velocimetry,PIV)试验%沟槽壁面%数值计算
泰勒渦動%粒子圖像測速技術(Particle image velocimetry,PIV)試驗%溝槽壁麵%數值計算
태륵와동%입자도상측속기술(Particle image velocimetry,PIV)시험%구조벽면%수치계산
Taylor vortex flow%particle image velocimetry(PIV) experiment%slit wall%numerical simulation
用粒子图像测速技术(Particle image velocimetry,PIV)对光滑壁面和沟槽数量为18的模型内的流场进行测量,初步获得沟槽的存在对于环隙内流场的影响规律;同时利用数值计算获得沟槽数量为18的模型内的流场分布,通过对比试验结果和数值模拟结果,验证数值计算方法可靠性。通过数值计算研究沟槽数量0、6、12、18模型内的流场分布,在比较沟槽模型与光壁模型环隙内的速度场和涡量场的基础上,得出以下结论:较少的沟槽数量增加了泰勒涡的轴向尺寸,随着沟槽数的增加,沟槽结构对流场影响不断加剧,环隙内最大径向速度和轴向速度均有不同程度的增加;对比不同轴向位置的流场分布,发现沟槽区域内存在明显的旋涡流动,不同轴向位置沟槽内的流体存在着进出环隙内的运动。
用粒子圖像測速技術(Particle image velocimetry,PIV)對光滑壁麵和溝槽數量為18的模型內的流場進行測量,初步穫得溝槽的存在對于環隙內流場的影響規律;同時利用數值計算穫得溝槽數量為18的模型內的流場分佈,通過對比試驗結果和數值模擬結果,驗證數值計算方法可靠性。通過數值計算研究溝槽數量0、6、12、18模型內的流場分佈,在比較溝槽模型與光壁模型環隙內的速度場和渦量場的基礎上,得齣以下結論:較少的溝槽數量增加瞭泰勒渦的軸嚮呎吋,隨著溝槽數的增加,溝槽結構對流場影響不斷加劇,環隙內最大徑嚮速度和軸嚮速度均有不同程度的增加;對比不同軸嚮位置的流場分佈,髮現溝槽區域內存在明顯的鏇渦流動,不同軸嚮位置溝槽內的流體存在著進齣環隙內的運動。
용입자도상측속기술(Particle image velocimetry,PIV)대광활벽면화구조수량위18적모형내적류장진행측량,초보획득구조적존재대우배극내류장적영향규률;동시이용수치계산획득구조수량위18적모형내적류장분포,통과대비시험결과화수치모의결과,험증수치계산방법가고성。통과수치계산연구구조수량0、6、12、18모형내적류장분포,재비교구조모형여광벽모형배극내적속도장화와량장적기출상,득출이하결론:교소적구조수량증가료태륵와적축향척촌,수착구조수적증가,구조결구대류장영향불단가극,배극내최대경향속도화축향속도균유불동정도적증가;대비불동축향위치적류장분포,발현구조구역내존재명현적선와류동,불동축향위치구조내적류체존재착진출배극내적운동。
The taylor vortex flow in the plain and slit 18 models is studied by experimental measurement, the preliminary effect of slit wall on the flow field in annular space is obtained. The flow field in the slit 18 model is also studied by numerical simulation. The reliability of numerical simulation is verified by comparing the experimental and numerical simulation results. The flow field in plain,slit 6, slit 12 and slit 18 model is studied by numerical simulation. The following conclusion is obtained by comparing the velocity and vorticity distribution in different models. The small number of slits in the outer cylinder changed the axial size of the Taylor vortex. As the increasing of the slit number, the effect of slit wall became more obvious, the maximize axial and radial velocity also increases as the increasing of slit number. The vortex flow is found in the slit wall by comparing the flow field in different axial positions, and the flow in the slit wall space has the tendency of moving in and out the annular space.