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Hohenemser, K. H. and Yin, Shen-Kuang, Some Applications of the Method of Multi-blade Coordinates, Journals of the American Society, Vol. 17, No. 3, July 1972, pp. 3-12. Coleman, R. P., of Self-Excited Mechanical Oscillations of Hinged Rotor Blades, NACA Advanced Restricted Rept. 3G29, Republished as Rept. 1351,1943, NACA. Miller, R. H., Helicopter Control and Stability in Hovering Flight, Journal of the Aeronautical Sciences, Vol. 15, No. 8, Aug. 1948, pp. 453-472. Azuma, A., Dynamic Analysis of the Rigid Rotor System, Journal of Aircraft, Vol. 4, No. 3, May-June 1967, pp. 203-209. Curtiss, H. C., Jr. and Shupe, N. K., Stability and Control Theory for Rotors, American 27th Annual National V/STOL Forum, Washington, D. C., May 1971. Ward, J. F., Exploratory Flight Investigation and Analysis of Structural Loads Encountered By A Rotor System, D-3676, Nov. 1966, NASA. Harris, F. D., Articulated Rotor Blade Flapping Motion at Low Advance Ration, Journal of the American Society, Vol. 17, No. 1, Jan. 1972, pp. 41-48. Ormiston, R. A. and Peters, D. A., Hingeless Rotor Response with Nonuniform Inflow and Elastic Blade Bending, Journal of Aircraft, Vol. 9, No. 10, Oct. 1972, pp. 730736.
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R. W. Paterson
Paul G. Vogt
Martin R. Fink
Journal of Aircraft
Hartford Financial Services (United States)
United Aircraft (Russia)
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Paterson et al. (Tue,) studied this question.
www.synapsesocial.com/papers/6a07e5f8f1d046f829735684 — DOI: https://doi.org/10.2514/3.60229