Now showing items 1-3 of 3
Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing
(Georgia Institute of Technology, 2004-12-01)
Aeroacoustic investigations regarding different types of helicopter noise have indicated that the most annoying noise is caused by impulsive blade surface pressure changes in descent or forward flight conditions. Blade ...
Helicopter blade-tip stability in forward flight
(Georgia Institute of Technology, 1971-08)
An analysis of the flutter and damping characteristics of helicopter rotors
(Georgia Institute of Technology, 1977-05)