A novel approach to structural load control using intelligent actuators [PDF]
The recent trend towards large multi-MW wind turbines resulted in the role of the control system becoming increasingly important. The extension of the role of the controller to alleviate structural loads has motivated the exploration of novel control ...
Dominguez, S.+4 more
core +1 more source
Are inclined screw blades for vertical grain augers advantageous? [PDF]
Due to modern technology, screw blades are often manufactured by rolling them out of one single strip of steel. When simultaneously some blade inclination is applied, less residual stresses and/or larger possible ratios between outer and shaft diameter ...
Rademacher, F.J.C.
core +2 more sources
Analysis of model rotor blade pressures during parallel interaction with twin vortices [PDF]
This paper presents and provides analysis of unsteady surface pressures measured on a model rotor blade as the blade experienced near parallel blade vortex interaction with a twin vortex system.
Beddoes T. S.+19 more
core +1 more source
Development of a regenerative pump impeller using rapid manufacturing techniques [PDF]
This paper presents a method of rapid manufacture used in the development of a regenerative pump impeller. Rapid manufacturing technology was used to create complex impeller blade profiles for testing as part of a regenerative pump optimisation process ...
Quail, Francis J.+2 more
core +1 more source
Influence of blade aerodynamic model on prediction of helicopter rotor aeroacoustic signatures [PDF]
Brown’s vorticity transport model has been used to investigate how the local blade aerodynamic model influences the quality of the prediction of the high-frequency airloads associated with blade–vortex interactions, and thus the accuracy with which the ...
Boyd D. D.+14 more
core +1 more source
Hingeless helicopter rotor with improved stability [PDF]
Improved stability was provided in a hingeless helicopter rotor by inclining the principal elastic flexural axes and coupling pitching of the rotor blade with the lead-lag bending of the blade.
Bousman, W. G.+3 more
core +1 more source
Radially extending rotor blades are disposed on a hub to form a supersonic propulsion fan for a turbofan engine. The peripheral spacing of the blades is such as to avoid forming a channel or passageway between adjacent blades.
Goldstein, A. W.
core +1 more source
Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [PDF]
The mid-span section of a previously reported controlled-diffusion compressor stator has been experimentally evaluated in cascade. Measurements are taken over a range of incidence angles for blade chord Reynolds numbers from 470,000 to 690,000.
Sanger, N. L., Shreeve, R. P.
core +1 more source
Development of an aeroelastic stability boundary for a rotor in autorotation [PDF]
<p>For the present study, a mathematical model AMRA was created to simulate the aeroelastic behaviour of a rotor during autorotation. Our model: Aeroelastic Model of a Rotor in Autorotation (AMRA) captures transverse bending and teeter ...
Gillies, E.A.+2 more
core
High resolution computation of the aerodynamics and acoustics of blade vortex interaction [PDF]
In the present work, high resolution CFD simulations have been performed on an idealised problem of the interaction of an independently generated vortex with a rotor blade, including a case where the vortex directly impacts on the blade.
Duraisamy, K., Thom, A.
core