Media Summary: Here we minimize the drag of a rectangular wing Structural weight minimization of a tubular spar composed of 6-DOF finite elements. We apply tip loads and allow the optimizer to ... Presented by Eytan Adler Find the paper here: In the past, ...
Aerodynamic Optimization Using Openaerostruct - Detailed Analysis & Overview
Here we minimize the drag of a rectangular wing Structural weight minimization of a tubular spar composed of 6-DOF finite elements. We apply tip loads and allow the optimizer to ... Presented by Eytan Adler Find the paper here: In the past, ... This shows the design variables that can be Two optimizations are shown: weight minimization (left) and fuel burn minimization (right). More details on this paper: ... Dr. John Jasa is the main developer of an open-source aerostructural
