A momentum analysis of helicopters and autogyros in inclined descent, with comments on operational restrictions
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[1] Quentin Wald. A Method for Rapid Estimation of Helicopter Performance , 1943 .
[2] Ludwig Prandtl,et al. Applications of Modern Hydrodynamics to Aeronautics , 1923 .
[3] Clarence D. Cone. A Theoretical Investigation of Vortex-Sheet Deformation Behind a Highly Loaded Wing and Its Effect on Lift , 1961 .
[4] G. J. Hancock. Comments on "Limiting Circulatory Lift of a Wing of Finite Aspect Ratio" , 1960 .
[5] Ir. J. Meijer Drees,et al. Airflow Patterns in the Neighbourhood of Helicopter Rotors , 1951 .
[6] John P Reeder,et al. On the Flying Qualities of Helicopters , 1949 .
[7] Alfred Gessow,et al. Flight Investigation of Effects of Rotor-Blade Twist on Helicopter Performance in the High-Speed and Vertical-Autorotative-Descent Conditions , 1948 .
[8] Julian Wolkovitch,et al. Analytical Prediction of Vortex-Ring Boundaries for Helicopters in Steep Descents , 1972 .
[9] Barnes W. McCormick. The Limiting Circulatory Lift of a Wing of Finite Aspect Ratio , 1959 .