F
Fred Nitzsche
Researcher at Carleton University
Publications - 94
Citations - 1402
Fred Nitzsche is an academic researcher from Carleton University. The author has contributed to research in topics: Helicopter rotor & Aeroelasticity. The author has an hindex of 19, co-authored 91 publications receiving 1150 citations. Previous affiliations of Fred Nitzsche include Aeronáutica & National Research Council.
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Dynamics, vibration and control of rotating composite beams and blades: A critical review
TL;DR: In this article, a comprehensive review of articles about rotating composite beams and blades is presented, which addresses analytical, semi-analytical and numerical studies dealing with dynamical problems involving adaptive/smart/intelligent materials (e.g., piezoelectric materials, electrorheological fluids, shape memory alloys, etc.), damping and vibration control, advanced composite materials, complicating effects and loadings, and experimental methods.
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Thermal properties of doubly reinforced fiberglass/epoxy composites with graphene nanoplatelets, graphene oxide and reduced-graphene oxide
TL;DR: In this paper, a novel manufacturing method based on VARTM was devised to incorporate carbon nanoparticles for the enhancement of thermal properties of multiscale laminates and the thermal, rheological and morphological properties of the resulting glass fiber-reinforced multi-scale composites were investigated.
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Evaluating Reynolds number effects in small-scale wind turbine experiments
TL;DR: In this paper, the effect of the Reynolds number on the initial wake expansion and on the thrust coefficient in scaled wind turbine tests was evaluated by using quantitative dye visualisation to identify the propagation of tip vortices downstream of the rotor.
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Application of Multi-Input Volterra Theory to Nonlinear Multi-Degree-of-Freedom Aerodynamic Systems
TL;DR: In this paper, a reduced-order-modeling approach for nonlinear, multi-degree-of-freedom aerodynamic systems using multi-input Volterra theory is presented.
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Development of the Smart Spring for Active Vibration Control of Helicopter Blades
TL;DR: Significant structural vibration is an undesirable characteristic in helicopter flight that leads to structural fatigue, poor ride quality for passengers and high acoustic signature for the vehicle as discussed by the authors, which is a common characteristic of helicopter flight.