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New model for rotor dynamics during pitch and roll of a hovering helicopter. Rosen, Aviv,Isser, Aharon. Journal of the American Helicopter Society . 1995
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Rotorcraft simulation model enhancement to support design, testing and operational analysis. Chengjian, He,Lee, C.S.,Chen, Weibin. Journal of the American Helicopter Society . 2000
[3]
Helicopter rotor dynamic inflow modeling for maneuvering flight. Krothapalli, Krishnamohan R.,Prasad, J.V.R.,Peters, David A. Journal of the American Helicopter Society . 2001
[4]
Validation of a real-time Engineering Simulation of the UH-60A Helicopter. Ballin,M.G. NASA-TM-88360 . 1987
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UH-60A black hawk engineering simulationprogram:Volume 1-Mathematical model. Howlett J J. NASA 166309 . 1981
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A mathematical model of the UH-60 helicop-ter. Hilbert K B. NASA TM-85890 . 1984
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Model of the unsteady aerodynamics of a hovering helicopter rotor that includes variations of the wake geometry. Rosen, Aviv,Isser, Aharon. Journal of the American Helicopter Society . 1995
[8]
Finite state induced flow models part II: three-dimensional rotor disk. Peters, David A.,He, Cheng Jian. Journal of Aircraft . 1995
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Development of a low-cost, multi-disciplinary rotorcraft simulation facility. Horn, Joseph F.,Bridges, Derek O.,Lopes, Leonard V.,Brentner, Kenneth S. Journal of Aerospace Computing, Information and Communication . 2005
[10]
Helicopter flight dynamic simulation with refined aerodynamics and flexible blade modeling. Theodore, Colin,Celi, Roberto. Journal of Aircraft . 2002