This project involves the optimal aerodynamic design of unmanned aerial vehicles (UAVs), making use of stateoftheart computational fluid dynamics and aerodynamic shape optimization techniques. The algorithm development will focus on modeling and exploiting laminarturbulent transition in the optimization cycle. The project should result in new and significantly improved aerodynamic shape optimization tools. This has the potential […]

Unmanned aerial vehicles (UAVs) provide a cost-effective and low-risk airborne platform for scientific and surveillance equipment. Due to the variety of instrumentation that they can carry, UAVs have enormous potential for use in a range of commercial and military sectors. However, their small size and low speed brings about aerodynamic challenges that are not present […]