UAV Design Assembly

grabcad

Continuation of a UAV design. 15 part assembly that uses simplified boxes for payloads used to estimate possible payload configurations and how mass properties change based on different setups. Further testing will go into wing spar testing and running the model through CFD to see how the down wash of the wing affects the tail lift coefficient. You can see the horizontal stabilizer is lower than the wing which is not common on aircraft, so it will be interesting to see how the wake of the wing affects.