Influence of Interactional Aerodynamics on Helicopter Rotor/Fuselage Coupled Response in Hover and Forward Flight

[1]  Peretz P. Friedmann,et al.  Recent developments in rotary-wing aeroelasticity , 1977 .

[2]  B. Maskew,et al.  Study for prediction of rotor/wake/fuselage interference, part 1 , 1985 .

[3]  Omri Rand,et al.  Model for investigation of helicopter fuselage influence on rotor flowfields , 1989 .

[4]  Peretz P. Friedmann,et al.  Formulation and solution of rotary-wing aeroelastic stability and response problems , 1983 .

[5]  Mark D. Betzina,et al.  Aerodynamic Loads Induced by a Rotor on a Body of Revolution , 1986 .

[6]  W. Johnson,et al.  Development and application of an analysis of axisymmetric body effects on helicopter rotor aerodynamics using modified slender body theory , 1984 .

[7]  David A. Peters,et al.  Coupled Rotor/Airframe Vibration Analysis By A Combined Harmonic - Balance, Impedance - Matching Method , 1980 .

[8]  Wayne Johnson,et al.  A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics. Part 1. Analysis Development , 1980 .

[9]  Donald L. Kunz Response Characteristics of a Linear Rotorcraft Vibration Model , 1981 .

[10]  A.R.S. Bramwell,et al.  A theory of the aerodynamic interference between a helicopter rotor blade and a fuselage and wing in hovering and forward flight , 1965 .

[11]  David T. Balch Experimental Study of Main Rotor/Tail Rotor/Airframe Interaction in Hover , 1983 .

[12]  Michael J Rutkowski The Vibration Characteristics of a Coupled Helicopter Rotor-Fuselage by a Finite Element Analysis. , 1983 .