This paper discusses the force history and flow topology of accelerating flat-plate wings. The work is a collaborative effort to study fundamental, unsteady low-Reynolds-number flows. The motion kinematics is designed to be relevant to the micro air vehicle flight regime. A combination of experimental and computational techniques is used to obtain data for comparison. There is a striking correlation of lift history data and flow topology from both experimental and computational data sets. It is found that the leading/trailing-edge vortex core separation during the initial part of a surge motion can be reasonably well approximated by , and the leading/trailing-edge vortex relative advection velocity is estimated to be . This leading/trailing-edge vortex relative advection velocity is a useful measure of how quickly the trailing-edge vortex moves away from the leading-edge vortex, which can influence lift for accelerating flat plates at high incidence angles.
Experiments and Computations on the Lift of Accelerating Flat Plates at Incidence
AIAA Journal ; 55 , 10 ; 3255-3265
2017-07-18
11 pages
Article (Journal)
Electronic Resource
English
Experiments and Computations on the Lift of Accelerating Flat Plates at Incidence
Online Contents | 2017
|Accelerating Scientific Computations Using FPGAs
British Library Conference Proceedings | 2006
|Accelerating Bio-Inspired MAV Computations using GPUs
AIAA | 2014
|Wind Tunnel Experiments and Navier-Stokes Computations of a High-Lift Military Airfoil
British Library Conference Proceedings | 1999
|Parametric Powered-Lift Navier-Stokes Computations
NTIS | 2004
|