Numerical analysis of the s1020 airfoils in tandem under different flapping configurations

The objective of this project is to improve the performance of the efficiency,thrust and lift of flapping wings in tandem arrangement.This research investigates the effect of the arrangement of the airfoils in tandem on the performance of the airfoils by varying the phase difference and distance between the airfoils.Three flapping configurations from an earlier phase of a research which gives high efficiency,thrust and lift are used in the tandem simulation.It is found all the different flapping configurati...