Kenneth W. McAlister
Airfoil interaction with an impinging vortex
3-D wake measurements near a hovering rotor for determining profile and induced drag
A pulse-forming network for particle path visualization
Devices that alter the tip vortex of a rotor
Devices that alter the tip vortex of a rotor / Kenneth W. McAlister, Chee Tung, James T. Heineck
NACA 0015 wing pressure and trailing vortex measurements
Suppression of dynamic stall with a leading-edge slat on a VR-7 airfoil
Water-tunnel experiments on an oscillating airfoil at RE = 21,000