论文信息 - Free Wake Model of Hovering Rotors Having Straight or Curved Blades - 字舞流文

Free Wake Model of Hovering Rotors Having Straight or Curved Blades

Aviv Rosen | Avinoam Graber

[1] Anton J. Landgrebe,et al. An Analytical and Experimental Investigation of Helicopter Rotor Hover Performance and Wake Geometry Characteristics , 1971 .

[2] F. X. Caradonna,et al. The structure of trailing vortices generated by model rotor blades , 1981 .

[3] J. Weissinger,et al. The Lift Distribution of Swept-Back Wings , 1947 .

[4] F. X. Caradonna,et al. Experimental and Analytical Studies of a Model Helicopter Rotor in Hover , 1980 .

[5] John Shaw,et al. Investigation of Aeroelastically Adaptive Rotors. , 1976 .

[6] A. Rosen,et al. Efficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices , 1984 .

[7] David R. Clark,et al. The Free Wake Analysis A Method For The Prediction Of Helicopter Rotor Hovering Performance. , 1969 .

[8] M. Scully,et al. Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads , 1975 .

[9] Kenneth L. Orloff,et al. Effect of Tip Shape on Blade Loading Characteristics and Wake Geometry for a Two-Bladed Rotor in Hover , 1980 .