Multiple-Wake Vortex Lattice Method for Membrane-Wing Kites Page 1 Multiple-Wake Vortex
Lattice Method for Membrane-Wing Kites Master of Science Thesis Presented for the degree …

The author presents an analysis on the development of Digital Image Correlation in various
applications including strain measurement. He discusses the concept of strain …

This paper describes a methodology to extract aerial vehicles' aerodynamic characteristics
from visually tracked trajectory data. The technique is being developed to study the …

An approach for predicting time varying aerodynamic loads on a pitching membrane wing
due to rotational pitching and steady airflow is presented. The proposed model utilizes …

To lessen the deterioration of fixed-wing aerodynamic performance associated with chord
Reynolds numbers below 100,000, flexible membrane wing designs have been studied and …

介绍了一种基于模型变形视频测量系统和计算空气动力学研究静弹性变形对气动力影响的方法.
利用模型变形视频测量系统获取模型在气动载荷作用下的静弹性变形, 驱动模型表面网格运动 …

在FL-26 跨声速风洞半模试验段进行了某高速飞机T 型尾翼颤振模型的光学测量实验,
并依据测量结果解算了尾翼颤振模型的弯扭特性. 颤振模型表面用白色圆点进行标记 …

Vortex-induced vibrations (VIVs) of a fixed two-dimensional perimeter-reinforced (PR)
membrane wing at 0 ≤ α 0≤ α Re (Reynolds number) ≤≤ 1000 and 0^ ∘ ≤ α 0∘≤ α …

Investigated and revealed are new insights into the individual, decoupled effects of induced
camber and spanwise bending on the lift, drag, and endurance for an optimum flexibility …

This paper presents a numerical investigation on the closed-loop performance of a two-
dimensional actuated membrane wing with fixed supports. The proposed concept mimics …