Modeling of unsteady aerodynamics for rotary-wing aeroelasticity

Mathematical and Computer Modelling - Tập 11 - Trang 293-297 - 1988
David A. Peters1
1School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0150, USA

Tài liệu tham khảo

Clark, 1969, The free-wake analysis--a mehod for the prediction of helicopter hovering performance, 25th Annual Forum of the AHS Friedmann,, 1985, Finite state modeling of unsteady aerodynamics and its application to a rotor dynamics problem, Eleventh European Rotorcraft Forum Gangwani, 1981, Prediction of dynamic stall and unsteady airloads for rotor blades, 37th Annual Forum of the AHS Gaonkar, 1986, Review of dynamic inflow modeling for rotorcraft flight dynamics, AIAA 27th SDM Conference Johnson,, 1980 Landgrebe, 1969, An analytical method for predicting rotor wake geometry, Journal of the American Helicopter Society, 14, 20, 10.4050/JAHS.14.20 Loewy, 1957, A two-dimensional approach to the unsteady aerodynamics of rotary wings, Journal of the Aerospace Sciences, 24, 82 McCroskey, 1981, The phenomenon of dynamic stall Peters, 1985, Application of various solution techniques to the calculation of transonic flutter boundaries, ASME Vibration and Sound Conference, Cincinnati Peters, 1987, The important of aerodynamics on dynamics, AHS National Specialists' Meeting on Aerodynamics and Acoustics Peters, 1987, A closed-form unsteady aerodynamic theory for lifting rotors in hover and forward flight, 43rd Annual National Forum of the American Helicopter Society Rogers, 1984, Applications of an analytic stall model to time-history and eigenvalue analysis of rotor blades, Journal of the American Helicopter, 29, 25, 10.4050/JAHS.29.25 Theodorsen, 1949, General theory of aerodynamic instabilities and the mechanism of flutter Tran, 1982, Semi-empirical model for the dynamic stall of airfoil in view of the application to the calculation of responses of a helicopter blade in forward flight, Vertica, 6, 219