[
[1] Prouty R.W., 1988, More Helicopter Aerodynamics, Phillips Pub Co.
]Search in Google Scholar
[
[2] Johnson W., 1980, Helicopter Theory, Princeton University Press, Princeton, New Jersey.
]Search in Google Scholar
[
[3] Padfield G.D., 1996, Helicopter Flight Dynamics. the Theory and Application of Flying Qualities and Simulation Modeling, Blackwell Publishing Ltd.
]Search in Google Scholar
[
[4] Warwick G., 1985, “Will rotors lose their bearings?”, Flight International, 29 June, no. 3966, vol.127, pp. 30-35.
]Search in Google Scholar
[
[5] Braun D., Frommlet H., Schwarz A., 1990, “FEL – A New Main Rotor System”, Vertica, Vol. 14, No. 1, pp. 47-60.
]Search in Google Scholar
[
[6] Schmit-Creton V., 2006, Successful Maiden Flight, Rotor on Line – A publication of Eurocopter, July/August, No. 67, from http://www.airbushelicopters.com/w1/jrotor/67
]Search in Google Scholar
[
[7] Wilson M., 1974, “Westland-Aerospatiale Lynx”, Flight International, 29 August, No. 3416, Vol. 106, Supplement 1, pp. 19-22.
]Search in Google Scholar
[
[8] Yeo H., Johnson W., 2005, “Comparison of Structural Loads Calculated Using Comprehensive Analysis”, 31st European Rotorcraft Forum, Florence, Italy, September 13-15.
]Search in Google Scholar
[
[9] Nguyen K., Lauzon D., Anand V., 1994, “Computation of Loads on the McDonnell Douglas Advanced Bearingless Rotor”, American Helicopter Society 50th Annual Forum, Washington D.C., May 11-13.
]Search in Google Scholar
[
[10] Gula P., Gorecki T., 2013,”Design, Experiments and Development of a Polish Unmanned Helicopter ILX-27”, 39th European Rotorcraft Forum, Moscow, Russia, 3-6 September.
]Search in Google Scholar
[
[11] Stanisławski J., 2015, “Pattern of Helicopter Rotor Loads and Blade Deformations in Some States of Flight Envelope”, Transactions of the Institute of Aviation, No.1(238), pp. 70-90.10.5604/05096669.1151311
]Search in Google Scholar
[
[12] Stanisławski J., 2016, “Simulation Investigation of Aerodynamic Effectiveness Reduction of Helicopter Tail Rotor”, Transactions of the Institute of Aviation, No.1(242), pp. 36-56.10.5604/05096669.1202201
]Search in Google Scholar
