نتایج جستجو برای: blade geometry

تعداد نتایج: 155053  

Journal: :International Journal of Turbomachinery, Propulsion and Power 2019

ژورنال: :مکانیک سازه ها و شاره ها 0
محسن به نیا دانشگاه صنعتی اصفهان مهدی نیلی احمدآبادی هیئت علمی/دانشگاه صنعتی اصفهان

the purpose of this study is to design a three-stage axial compressor with identical pressure ratio which makes an adequate pressure ratio and efficiency in design point conditions with rotational velocity of 38000rpm and mass flow rate of 3.2kg/s. first of all, considering some restrictions such as dehaller number more than 0.7 in all sections of the stator and the rotor, and relative mach num...

2011
Michael Lawson Ye Li

This paper describes the structural design of a tidal turbine composite blade. The structural design is preceded by two steps: hydrodynamic design and determination of extreme loads. The hydrodynamic design provides the blade external shape, i.e. the chord and twist distributions along the blade, which result in optimal performance of the tidal turbine over its lifetime. The extreme loads, i.e....

2006
Manuel A. Burgos Roque Corral Jaime Fernández-Castañeda Carlos López

The aerodynamic design of uncooled turbomachinery rows is based, among other things, on the repeated simulation of three-dimensional blade rows with a fast turnaround time. Traditionally blade rows have been simulated using clean aerodynamic surfaces and simplified computational domains consisting of just the aerodynamic surface and an approximated main annulus. A more accurate and realistic re...

2014
By H. Kim H. Lee D. Kim S. T. Bose D. A. Philips

A single rotor CFD model using wall-modeled Large Eddy Simulations (LES) was performed to predict the unsteady loading on the blade surface under partial admission. Geometry of the rotor blade of high pressure steam turbine of a 500 MW fossil-fuel power plant was used for this study. Periodically changing inlet boundary model was developed for single rotor model to simplify a full annular of th...

2008
Thanasis Barlas Jan-Willem van Wingerden Anton Hulskamp Gijs van Kuik

Wind tunnel tests on a non-rotating, dynamically scaled wind turbine blade equipped with variable trailing edge geometry were carried out. The effectiveness of the system for active load reduction purposes, with the interaction between structural dynamics, aerodynamics and control was tested. The actuation of the adaptive trailing edge was based on a piezoelectric bender actuator. The full aero...

2012
M. Rodríguez Ripoll B. Scheichl F. Franek Manel Rodríguez

Doctor blades are commonly used in paper machines in order to keep the surface of rollers clean. Due to higher demanding conditions, the requirements for doctor blades have steadily increased. The wear rates must remain low, while simultaneously their cleaning function has to be ensured. For this reason, the paper industry has developed a high degree of empirical knowledge concerning the cleani...

Journal: :Journal of colloid and interface science 1996
Spicer Keller Pratsinis

The effect of impeller type and shear rate on the evolution of floc size and structure during shear-induced flocculation of polystyrene particles with aluminum sulfate is investigated by image analysis. One radial flow (six-blade Rushton turbine) and two axial flow (three-blade fluid foil, four-blade 45° pitch) impeller configurations are examined. The steady state average floc size is show...

Computational fluid dynamics (CFD) is a powerful numerical tool that is becoming widely used to simulate many processes in the industry. In this work study of the stirred tank with 7 types of concave blade with CFD was presented. In the modeling of the impeller rotation, sliding mesh (SM) technique was used and RNG-k-ε model was selected for turbulence. Power consumption in various speeds in th...

The purpose of this study is to design a three-stage axial compressor with identical pressure ratio which makes an adequate pressure ratio and efficiency in design point conditions with rotational velocity of 38000rpm and mass flow rate of 3.2kg/s. First of all, considering some restrictions such as Dehaller number more than 0.7 in all sections of the stator and the rotor, and relative Mach num...

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