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- Pavel, M.D. (author), Schoones, M.M.J. (author) report 1999
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- Van Holten, TH. (author), Pavel, M.D. (author), Smits, G.N. (author) report 1999
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- Pavel, M.D. (author) report 1999
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- Pavel, M.D. (author) report 1999
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- Pavel, M.D. (author) doctoral thesis 2001
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- Brinkerink, N. (author), Pavel, M.D. (author) conference paper 2008
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- Pavel, M.D. (author), Padfield, G.D. (author) conference paper 2008
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- Dieterich, O. (author), Götz, J. (author), Vu, B. (author), Pavel, M.D. (author), Haverdings, H. (author), Jump, M. (author) conference paper 2008
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- Pavel, M.D. (author), Götz, J. (author), Vu, B. (author), Jump, M. (author) conference paper 2008
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- Jump, M. (author), Hodge, S. (author), Dang Vu, B. (author), Masarati, G. (author), Quaranta, G. (author), Mattaboni, M. (author), Pavel, M.D. (author), Dieterich, O. (author) conference paper 2008
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Pereira, R. (author), Schepers, G. (author), Pavel, M.D. (author)The aim of this study is to assess the load predicting capability of a classical Beddoes-Leishman dynamic stall model in a horizontal axis wind turbine (HAWT) environment, in the presence of yaw-misalignment. The dynamic stall model was tailored to the HAWT environment, and validated against unsteady thick airfoil data. Subsequently, the dynamic...conference paper 2011
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- Pavel, M.D. (author) conference paper 2011
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- Pavel, M.D. (author) book chapter 2011
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- Pavel, M.D. (author) book chapter 2012
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Dieterich, O. (author), Pavel, M.D. (author)For augmented helicopters with modern flight control systems, unintended and unexpected oscillations or divergences of the pilot-rotorcraft system have become an increasingly critical issue. Especially the rapid advances in the field of high response actuation and highly augmented flight control systems have increased the sensitivity to aspects...conference paper 2015
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Gori, R. (author), Gennaretti, M. (author), Pavel, M.D. (author), Stroosma, O. (author), Miletovic, I. (author)Among the many fundamental components of a flight simulator, the mathematical representation of the vehicle dynamics stands out for complexity and importance. This is especially true for helicopters, for which the complex dynamics involved prevents simple models to be sufficiently accurate without the need of a certain amount of artificial...conference paper 2015
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Wan, J. (author), Pavel, M.D. (author)The Ornicopter concept is a single-rotor, tailless configuration. By actively flapping its blades, the Ornicopter rotor can propel itself to rotate, and hence does not need a tail rotor. In previous research, the Ornicopter concept has been compared with the Bo-105 conventional helicopter from various aspects, while the Ornicopter has the same...journal article 2016
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Tod, G. (author), Pavel, M.D. (author), Malburet, F (author), Gomand, J (author), Barre, PJ (author)The paper reassesses the mechanism of biodynamical feedthrough coupling to helicopter body motion in lateral-roll helicopter tasks. An analytical bio-aeroelastic pilot–vehicle model is first developed and tested for various pilot’s neuromuscular adaptions in the lateral/roll axis helicopter tasks. The results demonstrate that pilot can...journal article 2016
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Dalmeijer, W. (author), Miletović, I. (author), Stroosma, O. (author), Pavel, M.D. (author)<br/>conference paper 2017
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Miletović, I. (author), Pool, D.M. (author), Stroosma, O. (author), Pavel, M.D. (author), Wentink, M (author), Mulder, Max (author)The fidelity of a rotorcraft flight simulator is influenced by many factors, such as the vehicle dynamic model and the motion cueing algorithm (MCA). To quantify the fidelity of a simulator objectively requires detailed knowledge of human pilot perception and control behaviour that is not yet available. As a consequence, subjective...conference paper 2017