Computational analysis of propulsive lift flapping wing model

Aviation is a fast growing and challenging field where demand for a better and economical technology is always sought of. The current research looks at a flapping-based vertical locomotion mechanism. The flapping wings combine lift and thrust functions, reducing drag-inducing structures. As a result, a high level of lift and hovering efficiency is required. The computational investigation of the aerodynamic efficiency of two-dimensional flat plates is carried out. An inverted V structure prototype, consisting of vertical hinged at their leading edges, is being considered. The effect of 2D plates is examined by adjusting the hole at different locations on the flapper. It has been discovered that a hole at a specific location with a specific geometry is needed for improved aerodynamic characteristics.