飞机尾流观测试验是研究飞机尾流演化耗散行为的基础. 受到不同大气环境的影响, 针对巡航,
进近等阶段的飞机尾流观测具备一定的挑战性. 本文综述了以风洞和拖曳水池为主的飞机尾流 …

We present experiments conducted in a wind tunnel to characterize yaw angle effects on the
drag force acting on the Ahmed body with slant angle of 25°. The main contribution of this …

Small-scale drones have enough sensing and computing power to find use across a
growing number of applications. However, flying in the low–Reynolds number regime …

An experimental method for determination of aerodynamic loads is presented. It is based on
velocity vector field results obtained with Particle Image Velocimetry (PIV). As PIV is an …

This work provides an inclusive nonlinear aeroelastic study on the effects of horizontal axis
Small-Scale Wind Turbines (SSWTs)'s preset angle of attack as well as aspect ratio on its …

Over the last 10 years, the use of micro air vehicles has rapidly covered a broad range of
civilian and military applications. While most missions require optimizing the endurance, a …

The capability of an oscillating trailing edge flap to enhance the lift generated by a rigid
NACA-0012 airfoil at 2. 1× 1 0 4 Reynolds number is investigated. Experiments are …

Inspired by the efficiency of soaring birds in crossing very large distances with barely flap
their wings, this work presents a simple model of UAV that, adopting the capabilities of these …

The lift coefficient for a flat plate at low angles of attack is obtained experimentally for various
aspect ratios (AR​=​ 1, 2, 4, 8) and moderate Reynolds numbers (Re​=​ 40​×​ 10 3 to …

We present a detailed analysis of experimental and numerical results for the flow of trailing
vortices behind a NACA0012 wing model. Particular attention is paid to a specific value of …