前端襟翼对带涡襟翼的细长翼影响的实验研究  

AN EXPERIMENTAL STUDY ON THE EFFECTIVENESS OF APEX-FLAP ON VORTEX-FLAPPED SLENDER WING

作　　者：郭文海[1] 忻鼎定[2] 庄逢甘[2] 

机构地区：[1]中国科学院力学研究所,北京100080 [2]北京航空航天大学流体力学研究所,北京100083

出　　处：《航空学报》1993年第8期B389-B393,共5页Acta Aeronautica et Astronautica Sinica

摘　　要：为改善带涡襟翼的细长翼的升阻特性,在其上附加了前端襟翼和后缘襟翼。通过前端涡(前端襟翼上产生)和前缘涡(涡襟翼上产生)相互作用对气动特性影响的研究,得到能够改善升阻特性的方法。结果表明,涡的相互作用对涡的产生和发展有很大影响,因而影响细长翼气动特性。附加前端襟翼和后缘襟翼是必要的。由此得到既能增升又能减阻的前端襟翼偏转角。In order to improve the aerodynamic characteristics of vortex-flapped slonder wings, the apex-flap and trailing-edge flaps are added on them. Through studying the interaction between apex vortices and leading-edge vortices, a way is found to improve the aerodynamic characteristics of slender wings. Results show that the vortical interaction has a great influence on vortical production, movement and aerodynamic characteristics of slender wings. By controlling the deflected angle of the apex flap, the drag will be reduced and the lift increased. So the method of employing apex flap and trailing-edge flaps in combination is effective in enhancing the aerodynamic characteristics of slender wings.

关 键 词：减阻 涡襟翼 细长翼 空气动力学 

分 类 号：V211.41[航空宇航科学与技术—航空宇航推进理论与工程]