Grant

A Combined Approach for Investigating the Effects of Large Wing Sweep and Unsteady Wing Motion on Transition and Separation: Flight Experiments, Wind Tunnel Experiments and Simulations

Sponsored by Air Force Office of Scientific Research

Active

$320K Funding

1 People

External

Related Topics

aerodynamics, flight testing, wing motion, wind tunnel testing, fluid dynamics

People

Hermann Fasel
Principal Investigator (PI)
Aerospace and Mechanical Engineering﹒Professor