1. The aerodynamic optimisation of a low-Reynolds paper plane with adjoint method
- Author
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Xinxin Zhang, Yang Zhang, and George Chen
- Subjects
Airfoil ,020301 aerospace & aeronautics ,Drag coefficient ,Computer simulation ,Aerospace Engineering ,Stall (fluid mechanics) ,02 engineering and technology ,Aerodynamics ,Solver ,01 natural sciences ,010305 fluids & plasmas ,0203 mechanical engineering ,Control theory ,0103 physical sciences ,Wingtip device ,Mathematics - Abstract
The aerodynamic performance of a deployable and low-cost unmanned aerial vehicle (UAV) is investigated and improved in present work. The parameters of configuration, such as airfoil and winglet, are determined via an optimising process based on a discrete adjoint method. The optimised target is locked on an increasing lift-to-drag ratio with a limited variation of pitching moments. The separation that will lead to a stall is delayed after optimisation. Up to 128 design variables are used by the optimised solver to give enough flexibility of the geometrical transformation. As much as 20% enhancement of lift-to-drag ratio is gained at the cruise angle-of-attack, that is, a significant improvement in the lift-to-drag ratio adhering to the preferred configuration is obtained with increasing lift and decreasing drag coefficients, essentially entailing an improved aerodynamic performance.
- Published
- 2020