Results 51 to 60 of about 32,908 (214)

Wind Turbine Blade Structural Efficiency [PDF]

open access: yes, 2012
Alternative structural layouts for wind turbine blades are investigated with the aim to improve their design, minimize weight and reduce the cost of wind energy.
Bendsøe M. P.   +10 more
core   +2 more sources

Effect of V-shaped Ribs on Internal Cooling of Gas Turbine Blades [PDF]

open access: yes, 2017
Thermal efficiency and power output of gas turbines increase with increasing turbine rotor inlet temperature. The rotor inlet temperatures in most gas turbines are far higher than the melting point of the blade material.
Kamat, H. (Harishkumar)   +2 more
core   +2 more sources

Influence of Thermodynamic Effect on Blade Load in a Cavitating Inducer

open access: yesInternational Journal of Rotating Machinery, 2010
Distribution of the blade load is one of the design parameters for a cavitating inducer. For experimental investigation of the thermodynamic effect on the blade load, we conducted experiments in both cold water and liquid nitrogen.
Kengo Kikuta   +5 more
doaj   +1 more source

Aeroelastic Characteri stics of Rotor Blades with Trailing Edge Flaps

open access: yesInternational Journal of Aeronautical and Space Sciences, 2007
The aeroelastic analysis of rotor blades with trailing edge flaps, focused on reducing vibration while minimizing control effort, are investigated using large deflection-type beam theory in forward flight. The rotor blade aerodynamic forces are calculated using two-dimensional quasi-steady strip theory. For the analysis of forward flight, the nonlinear
Lim, IG Lim, In-Gyu, Lee, I Lee, In
openaire   +2 more sources

Numerical Studies on a NACA0018 Airfoil Blade HAWT with Trailing Edge Jet Flow

open access: yesE3S Web of Conferences, 2018
This study analyzed an airfoil blade for a horizontal-axis wind turbine (HAWT) with a trailing-edge jet flow design. This design was realized by drilling a hole in the trailing edge of an NACA0018 blade of a conventional HAWT to serve as a pressure ...
Uzu-Kuei Hsu   +3 more
doaj   +1 more source

Aerodynamic noise from rigid trailing edges with finite porous extensions

open access: yes, 2017
This paper investigates the effects of finite flat porous extensions to semi-infinite impermeable flat plates in an attempt to control trailing-edge noise through bio-inspired adaptations.
Ayton, L. J., Kisil, A. V.
core   +1 more source

Numerical Investigation on Pressure Fluctuations for Different Configurations of Vaned Diffuser Pumps

open access: yesInternational Journal of Rotating Machinery, 2007
Numerical simulations on impeller-diffuser interactions in radial diffuser pumps are conducted to investigate the unsteady flow, and more attention is paid to pressure fluctuations on the blade and vane surfaces ...
Jianjun Feng   +2 more
doaj   +1 more source

Modeling and Measurement Study for Wind Turbine Blade Trailing Edge Cracking Acoustical Detection

open access: yesIEEE Access, 2020
The rapid deployment of the offshore wind turbine technology has brought more requirements for remote turbine health monitoring especially for blade health conditions.
Yang Zhang   +3 more
doaj   +1 more source

Effect of trailing edge geometry and thickness on the performance of certain turbine stator blading [PDF]

open access: yes
The experimental and analytical investigation included solid blades with five different trailing-edge thicknesses and four different trailing-edge geometries.
Helon, R. M., Prust, H. W., Jr.
core   +1 more source

Trailing Edge Loss of Choked Organic Vapor Turbine Blades

open access: yesInternational Journal of Turbomachinery, Propulsion and Power
The present study reports the outcome of an experimental study of organic vapor trailing edge flows. As a working fluid, the organic vapor Novec 649 was used under representative pressure and temperature conditions for organic Rankine cycle (ORC) turbine applications characterized by values of the fundamental derivative of gas dynamics below unity.
Leander Hake, Stefan aus der Wiesche
openaire   +1 more source

Home - About - Disclaimer - Privacy