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Unsteady Aerodynamic Analysis of a 2D Flapping Airfoil Performing Lateral Motion
International Research Journal of Engineering and Technology
In the current scenario, Nano Air Vehicle (NAV) plays an indispensable role in both defence and civil applications significantly, such as earthquake, avalanche, low intensity conflict, spying, etc. The important features of NAV include low Reynolds Number, fluid-solid interaction, boundary layer separation and other parameters. This research work is the continuation of our previous work related to the aerodynamics of flexible flapper & passive stability (200 mm flying model) and fully unsteadyfatcat:7qlqfiq7dzcbxhmzr7b7kwnouq