The Impact of Flapping Trajectories on the Induced Thrust of a Single and Tandem Configuration Flapping Foil
Azad Duppala, Ajay Kumar, Venkata Ramana Menda, Prafulla Kumar Swain, Srinivas Vadapalli, Divakar Bommana
Abstract
Azad Duppala, Ajay Kumar, Venkata Ramana Menda, Prafulla Kumar Swain, Srinivas Vadapalli, Divakar Bommana
Abstract
Abstract The development of propulsion devices by using the propulsive mechanisms of aquatic animals such as fish is a challenging task. An attempt has been made to replicate the fishtailed motion that caused thrust in the current investigation. At a low Reynolds number of Re = 1173, the propulsive performance of National Advisory Committee for Aeronautics 0012 flapping foils enduring distinct flapping trajectories (fishtailed and elliptical) is evaluated. A dynamic mesh arbitrary Lagrangian–Eulerian framework is used to understand the desired flapping motion of the foils while solving the flow via incompressible Navier–Stokes equations. Along with the flapping trajectory, the effects of the Strouhal number (St), inter-foils distance (Lx), and phase angle (φ) between the foils on the produced thrust are examined. The results demonstrate that using tandem configuration flapping foil with elliptical and fishtailed flapping can significantly increase the induced thrust and propulsive efficiency.
OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Abstract The development of propulsion devices by using the propulsive mechanisms of aquatic animals such as fish is a challenging task. An attempt has been made to replicate the fishtailed motion that caused thrust in the current investigation. At a low Reynolds number of Re = 1173, the propulsive performance of National Advisory Committee for Aeronautics 0012 flapping foils enduring distinct flapping trajectories (fishtailed and elliptical) is evaluated. A dynamic mesh arbitrary Lagrangian–Eulerian framework is used to understand the desired flapping motion of the foils while solving the flow via incompressible Navier–Stokes equations. Along with the flapping trajectory, the effects of the Strouhal number (St), inter-foils distance (Lx), and phase angle (φ) between the foils on the produced thrust are examined. The results demonstrate that using tandem configuration flapping foil with elliptical and fishtailed flapping can significantly increase the induced thrust and propulsive efficiency.
Key concepts: Flapping, Thrust, FOIL method, Tandem, Aerospace engineering, Physics, Aeronautics, Engineering