典型文献
Lift enhancement based on virtual aerodynamic shape using a dual synthetic jet actuator
文献摘要：
The Dual Synthetic Jet Actuator(DSJA)is used to develop a new type of lift enhance-ment device based on circulation control,and to control the flow over the two-dimensional(2D)NACA0015 airfoil.The lift enhancement device is composed of a DSJA and a rounded trailing edge(Coanda surface).The two outlets of the DSJA eject two jets(Jet 1 and Jet 2).Jet 1 ejects from the upper trailing edge,which increases the circulation of airfoil with the help of the Coanda surface.Jet 2 ejects from the lower trailing edge,which acts as a virtual flap.The Reynolds number based on the airfoil chord length and free flow velocity is 250000.The results indicate that the circulation control method based on Dual Synthetic Jet(DSJ)has good performance in lift enhancement,whose con-trol effect is closely related to momentum coefficient and reduced frequency.With the increase of the reduced frequency,the control effect of the lift enhancement is slightly reduced.As the momen-tum coefficient increases,the control effect becomes better.When the angle of attack is greater than 4°,the increments of lift coefficients under the control of DSJ are larger than those under the con-trol of the steady blowing at a same momentum coefficient.The maximum lift augmentation effi-ciency can reach 47 when the momentum coefficient is 0.02,which is higher than the value in the case with steady blowing jet circulation control.
文献关键词：
中图分类号：
作者姓名：
Shiqing LI;Zhenbing LUO;Xiong DENG;Zhiyong LIU;Tianxiang GAO;Zhijie ZHAO
作者机构：
College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China
文献出处：
引用格式：
[1]Shiqing LI;Zhenbing LUO;Xiong DENG;Zhiyong LIU;Tianxiang GAO;Zhijie ZHAO-.Lift enhancement based on virtual aerodynamic shape using a dual synthetic jet actuator)[J].中国航空学报（英文版）,2022(12):117-129
A类：
DSJA,eject,ejects,momen
B类：
Lift,enhancement,virtual,aerodynamic,shape,using,dual,synthetic,actuator,Dual,Synthetic,Jet,Actuator,is,used,develop,new,type,lift,device,circulation,control,flow,over,two,dimensional,2D,NACA0015,airfoil,composed,rounded,trailing,edge,Coanda,surface,outlets,jets,from,upper,which,increases,help,lower,acts,flap,Reynolds,number,chord,length,free,velocity,results,indicate,that,method,has,good,performance,whose,effect,closely,related,momentum,reduced,frequency,With,slightly,becomes,better,When,angle,attack,greater,than,increments,coefficients,under,are,larger,those,steady,blowing,same,maximum,augmentation,ciency,can,reach,when,higher,value,case
AB值：
0.427062
相似文献
机标中图分类号，由域田数据科技根据网络公开资料自动分析生成，仅供学习研究参考。
