Instructor: Thomas M. Hermann
Biography: Thomas M. Hermann has a strong background in aeroelastic analysis of aerospace structures and has performed structural dynamic, aeroelastic, and dynamic loads analysis of aircraft ranging from single engine general aviation aircraft to twin turboprop, carrier based, AEW aircraft to twin turbofan transports and business jets. In the course of these projects, he has also conducted ground vibration and flight flutter testing. He completed his master's thesis in transonic aeroelasticity at the University of Kansas under Dr. C. Edward Lan. Courses taught by this instructor: Principles of Aeroelasticity |