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INVESTIGATION OF MECHANISM OF WIDENED STEADY WORKING RANGE FOR SKEWED-SWEPT ROTATING BLADES
Author: ZouTieFeng
Tutor: CaiNa
School: North China Electric Power University
Course: Power Engineering
Keywords: Swept rotor blades Numerical Simulation NND scheme Radial pressure gradient The expanding stable machine management
CLC: TB126
Type: Master's thesis
Year: 2001
Downloads: 98
Quote: 0
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Abstract
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The bend of the paper with the same geometric structure parameters and aerodynamic parameters swept rotor and radial dynamic leaves , aerodynamic flow field calculation , the purpose is to reveal swept automatically the leaf blower expand the stable operating range mechanism . Through the analysis of the calculation results , swept rotor blades using change factors play a decisive role in the entire flow field - radial pressure gradient . Radial pressure gradient essentially led to changes in the structure of the flow field , a change in the flow parameters . Will calculate the results of the efficiency of the rotor blades , pressure rise , and the export flow angle , loss and average pressure ratio along the blade distribution with the experimental results , high precision calculations , the use of the numerical model is reasonable , be able to simulate the reliable cascade of internal flow field . Stable conditions the aerodynamic calculation swept move cascade broaden the operating range of the mechanism analysis provides a theoretical basis . This article is the three Wei Leinuo average Navier-Stokes equations , and several high-resolution format a comparative analysis , the final selection of the calculation NND format for high-precision format , application no matrix inversion LU-SGS implicit algorithm to solve the equation . The use of the LU-SGS algorithm greatly improves the speed of convergence of the numerical calculation of the turbulent flow field , swept move Yesan Wei viscous flow field complex and time-consuming flow numerical simulation of good performance in both accuracy and computational efficiency . . Radial dual actuator disk theory model masterpiece amended to make it more in line with the swept rotor blades liquidity situation . Also were swept rotor blades and radial design of the rotor blades , select reasonable parameters , the use of isolated airfoil theory to carry out aerodynamic blade design the structure of the blade . And the the swept angle values ??and different center of gravity line of the aerodynamic performance of the rotor blades , and select the appropriate the swept angle values ??and focus line . Finally, consider the movement leaves the match , the prospect of the swept rotor blade optimization design .
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CLC: > Industrial Technology > General industrial technology > Engineering and basic science > Engineering Mechanics > Engineering Fluid Mechanics
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