航空工程进展
航空工程進展
항공공정진전
ADVANCES IN AERONAUTICAL SCIENCE AND ENGINEERING
2014年
3期
320-325
,共6页
赵曙%朱惠人%郭涛%许都纯
趙曙%硃惠人%郭濤%許都純
조서%주혜인%곽도%허도순
带肋通道%旋转%对流传热%压力系数
帶肋通道%鏇轉%對流傳熱%壓力繫數
대륵통도%선전%대류전열%압력계수
ribbed channel%rotating%convective heat transfer%pressure coefficient
为了深入了解旋转作用对回转内通道换热特征的影响,采用三维数值模拟方法研究旋转数、旋转半径对带肋内通道模型的流动换热影响。通道入口雷诺数为1.7×104、旋转数范围为0~0.09,出口1、出口2、出口3的质量流量分配比为1∶2∶1,旋转半径与水力直径之比的范围为0~69.6。结果表明:旋转作用力使径向出流通道的压力系数逐渐增大,径向入流通道的压力系数迅速减小;径向出流通道后缘面的努赛尔数( N u)随旋转数增加而增大,径向入流通道后缘面的 Nu随旋转数增加而减小,前缘面 Nu随旋转数变化情况相反;前、后缘面 Nu沿流向均随旋转半径与水力直径比的增加略有增大,旋转半径变化对壁面换热影响较小。
為瞭深入瞭解鏇轉作用對迴轉內通道換熱特徵的影響,採用三維數值模擬方法研究鏇轉數、鏇轉半徑對帶肋內通道模型的流動換熱影響。通道入口雷諾數為1.7×104、鏇轉數範圍為0~0.09,齣口1、齣口2、齣口3的質量流量分配比為1∶2∶1,鏇轉半徑與水力直徑之比的範圍為0~69.6。結果錶明:鏇轉作用力使徑嚮齣流通道的壓力繫數逐漸增大,徑嚮入流通道的壓力繫數迅速減小;徑嚮齣流通道後緣麵的努賽爾數( N u)隨鏇轉數增加而增大,徑嚮入流通道後緣麵的 Nu隨鏇轉數增加而減小,前緣麵 Nu隨鏇轉數變化情況相反;前、後緣麵 Nu沿流嚮均隨鏇轉半徑與水力直徑比的增加略有增大,鏇轉半徑變化對壁麵換熱影響較小。
위료심입료해선전작용대회전내통도환열특정적영향,채용삼유수치모의방법연구선전수、선전반경대대륵내통도모형적류동환열영향。통도입구뢰낙수위1.7×104、선전수범위위0~0.09,출구1、출구2、출구3적질량류량분배비위1∶2∶1,선전반경여수력직경지비적범위위0~69.6。결과표명:선전작용력사경향출류통도적압력계수축점증대,경향입류통도적압력계수신속감소;경향출류통도후연면적노새이수( N u)수선전수증가이증대,경향입류통도후연면적 Nu수선전수증가이감소,전연면 Nu수선전수변화정황상반;전、후연면 Nu연류향균수선전반경여수력직경비적증가략유증대,선전반경변화대벽면환열영향교소。
To better understand the effects of rotation on the internal channel heat transfer characteristics ,the flow and heat transfer condition in an internal channel with 90° ribs are investigated using three-dimensional nu-merical simulation method .The inlet Reynolds number is 1.7×104 and three outlets mass flow discharge ratio is 1∶2∶1 .The Rotating number and the hydraulic diameter divided by radius of gyration range from 0 to 0.09 and 0 to 69.6 ,respectively .The influence of Rotation number and Radius of gyration on heat transfer coefficient were achieved .Results show that the pressure coefficient increases along radial outflow and decreases along ra-dial inflow due to rotational force;in the trailing surface ,Nusselt number(Nu) in radial outflow passages in-creases and the Nu in radial inflow passage decreases with the augment of the rotation number ,the variation of Nu in the leading surface contrary to that of the trailing surface;the Nu along the flow direction in trailing and leading surface are slightly enhanced when gyration radius to hydraulic diameter ratio increase ,the surface heat transfer coefficient is affected on the variable radius of gyration.