p.138
p.142
p.147
p.151
p.156
p.160
p.164
p.168
p.172
Drag Reduction on the 35° Slant Angle Ahmed Reference Body Using Flaps
Abstract:
Based on computational fluid dynamics numerical simulation methods, this article studied the changes of resistance characteristics and tail pressure distribution on the 35° slant angle Ahmed model after installing the rear flaps. The results show that the appropriate size and reasonable arrangement of flaps can make the model tail separated airflow attach on the flap and the flap trailing edge separate again, narrow the tail separation zones, improve the model tail pressure, reduce the pressure difference on the forepart and rear model,lower the model resistance, then causing the drag reduction effect. The study found that the best drag reduction effect is to use 50 mm high flap, decorate in the rear bevel edge from Ahmed model 15 mm, the largest model resistance can be reduced by 5.37%.
Info:
Periodical:
Pages:
156-159
Citation:
Online since:
October 2014
Authors:
Keywords:
Price:
Сopyright:
© 2014 Trans Tech Publications Ltd. All Rights Reserved
Share:
Citation: