This paper presents the results of a recent investigation into the vortex structure over a
nonslender delta wing with leading edge sweep, Λ= 50. A flow visualisation study in water …

Scale effect is of significance in all experimental aerodynamics testing. At high angles of
attack such issues as Reynolds and Mach number scaling are further complicated by the …

Current and future fixed-wing micro air vehicles (MAVs) exhibit a variety of separated and
vortex-dominated flow fields including tip vortices, leading-edge vortices, vortex shedding …

The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with
sweep angle of 45 degree is characterized in a low-speed wind tunnel using laser …

The colonization of the pelagic realm by the vertebrates represents one of the major
transitions in the evolutionary success of the group and in the establishment of modern …

摘要针对低雷诺数微型飞行器的气动布局, 设计出类似雨燕翅膀的一组具有不同前缘钝度的中等
后掠($\varLambda= 50^{\circ} $) 仿生三角翼. 为了定量对比研究三角翼后缘收缩产生的气动 …

EARLY ight endeavors led to the prominence of the multiplane configuration. The moderate
lifting performance and structural integrity of early ying machines found redemption in the …

A low-speed wind tunnel investigation was conducted to characterize the performance of
plain and Gurney flaps on a 55 deg sweep delta wing. The geometry of the plain trailing …

Water tunnels are emerging as a possible useful alternative to small low-speed wind tunnels
for an expanded range of aerodynamic testing. In this report, an assessment is made …

A low speed wind tunnel investigation was conducted to examine the effect of a pusher
propeller on a 65 deg sweep delta wing. Two different propeller diameters were evaluated …