%0 Journal Article
%T Thrust Optimization of Flapping Wing via Gradient Descent Technologies
%A Jeshwanth Kundem
%J Open Journal of Fluid Dynamics
%P 83-99
%@ 2165-3860
%D 2024
%I Scientific Research Publishing
%R 10.4236/ojfd.2024.142004
%X The current work aims at employing a gradient descent algorithm for optimizing the thrust of a flapping wing. An in-house solver has been employed, along with mesh movement methodologies to capture the dynamics of flow around the airfoil. An efficient framework for implementing the coupled solver and optimization in a multicore environment has been implemented for the generation of optimized solutions—maximizing thrust performance & computational speed.
%K Steepest Descent
%K CFD
%K Flapping Wing Airfoil
%K Thrust Performance
%U http://www.scirp.org/journal/PaperInformation.aspx?PaperID=133435