Adjoint-based drag reduction for M.Tech thesis using SU2/ADE. Improved cruise efficiency by 15%.
Based on given wing deimension utilize the spreadsheet calculation and get the spar sizing and wing airfoil proper placement. Then using solidworls perofrm design and part fea simulation.
Conceptual design: Payload 30 kg, 500 km range, 30 min loiter, Pneumatically-launched take off, 10000 meters, parachute landing, jet prop, 0.7 mach cruise, constraint analysis Python tool.