نتایج جستجو برای: rotor blade

تعداد نتایج: 23793  

2007
Anton W. Hulskamp Adriaan Beukers Harald E.N. Bersee Jan Willem van Wingerden

Within wind energy research there is a drive towards the development of a “smart rotor”; a rotor of which the loading can be measured and controlled through the application of a sensor system, a control system and an aerodynamic device. Most promising solutions from an aerodynamic point of view are trailing edge flaps, either hinged or continuously deformable. An experiment was considered neces...

Journal: :Journal of physics 2022

Abstract In order to investigate the noise characteristics of open rotor, numerical simulation was performed for an rotor which contains 11 blades front row and 9 rear row. The aerodynamic compared with a single propeller, i.e. propeller. Numerical results show that predicted field agree well literature. spectrum is obviously more complex higher than addition, contribution different generation ...

2015
Aaron Rosenberg Anupam Sharma

This paper extends the prescribed wake vortex lattice/line method (VLM) to perform aerodynamic analysis and optimization of dual-rotor wind turbines (DRWTs). A DRWT turbine consists of a large, primary rotor placed co-axially behind a smaller, secondary rotor. The additional vortex system introduced by the secondary rotor of a DRWT is modeled while taking into account the singularities that occ...

Journal: :DEStech Transactions on Environment, Energy and Earth Sciences 2018

Journal: :Ist International Surface Technology 2021

2013
Michael Mayo Rafael Lozano Vrishank Raghav Narayanan Komerath

Rotating blades on helicopters experience reverse flow under high advance ratio conditions. Here, reverse flow is characterized by the flow traveling from the sharp trailing edge to the blunt leading edge. Uncertainty in the blade aerodynamic loads under these conditions has been a limitation during the design of high-speed rotorcraft. In this work, we hypothesize that the reverse flow over a y...

2013
Matthew Lackner Jaime Peraire

High cycle fatigue (HCF) cracks generated by compressor blade vibrations are a common source of failure in gas turbine engines. Current methods for crack detection are costly, time consuming, and prone to errors. In-situ blade vibration detection would help operators avoid critical engine speeds, and help infer the presence of cracks via a change in the mode of a blade. Blade vibrations can be ...

2012

This paper presents a numerical analysis of the performance of a five-bladed Darrieus vertical-axis water turbine, based on the NACA 0025 blade profile, for both bare and shrouded configurations. A complete campaign of 2-D simulations, performed for several values of tip speed ratio and based on RANS unsteady calculations, has been performed to obtain the rotor torque and power curves. Also the...

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