D
Dean T. Mook
Researcher at Virginia Tech
Publications - 112
Citations - 3129
Dean T. Mook is an academic researcher from Virginia Tech. The author has contributed to research in topics: Nonlinear system & Aerodynamics. The author has an hindex of 30, co-authored 112 publications receiving 2978 citations.
Papers
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Journal ArticleDOI
An overview on non-ideal vibrations
José Manoel Balthazar,José Manoel Balthazar,Dean T. Mook,Hans Ingo Weber,Reyolando M. L. R. F. Brasil,A. Fenili,D. Belato,Jorge Luis Palacios Felix +7 more
TL;DR: In this paper, the dynamical coupling between energy sources and structural response is analyzed for real motors, since real motors have limited output power, and it must not be ignored in real engineering problems.
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Theoretical and experimental study of modal interaction in a two-degree-of-freedom structure
TL;DR: In this article, an experimental and theoretical investigation has been made of the primary resonances of the system, which occur when the frequency of excitation is near one of the natural frequencies, ω 1 and ω 2.
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A refined nonlinear model of composite plates with integrated piezoelectric actuators and sensors
TL;DR: In this paper, a fully nonlinear theory for the dynamics and active control of elastic laminated plates with integrated piezoelectric actuators and sensors undergoing large-rotation and small-strain vibrations is presented.
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On methods for continuous systems with quadratic and cubic nonlinearities
TL;DR: It is shown by means of a simple example that perturbation and computational methods based on first discretizing the systems may lead to erroncous results whereas perturbations methods that attack directly the nonlinear partial-differential equations and boundary conditions avoid the pitfalls associated with the analysis of the discretized systems.
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Analytical study of the subsonic wing-rock phenomenon for slender delta wings
TL;DR: In this article, an analytic expression describing the aerodynamic roll moment has been obtained from the numerical simulation of wing rock, which is used in the equation governing the rolling motion of a delta wing around its midspan axis.