Now showing items 1-4 of 4
(World Scientific, 1987)
(American Helicopter Society, 1989)An active control system to suppress the response of the blade bending modes of a tilt-rotor aircraft to axial gusts and wing/rotor interference is described. The use of blade-mounted accelerometers as sensors is shown to ...
(Elsevier Science, 1988)The present paper illustrates a series of theoretical results on non-equilibrium phonon effects based on a novel Monte Carlo algorithm. No assumptions on the form of the phonon or the electron distributions are required. ...