According to a certain type of flying in the no imitation gull wing design straight wing with man. Then the bionic wing and conventional airfoil are simulated, and compared the two kinds of wing aerodynamic parameters. The study found, hale no flow man-machine bionic wing design can effectively improve the wing, reduce the upper wing surface flow separation, reduce the lift loss, reduce the pressure drag, improve the lift drag ratio of the wings. In this paper, the simulation results for the design of the UAV wing provides certain reference.
Analysis of the Bionic Wing's Aerodynamic Performance
Applied Mechanics and Materials ; 644-650 ; 385-389
2014-09-22
5 pages
Article (Journal)
Electronic Resource
English
ENGINEERING NOTES - Improvement of a Wing's Aerodynamic Efficiency Using Coanda Tip Jets
Online Contents | 2000
|Online Contents | 1994
Rotor & Wing's Helicopter Heroism Award
Online Contents | 1996
Rotor & Wing's - Annual Supplier Sourcebook 2005
Online Contents | 2004
British Library Conference Proceedings | 2022
|