Please use this identifier to cite or link to this item: http://148.72.244.84:8080/xmlui/handle/xmlui/13125
Title: COMPUTER PROGRAM TO PREDICT PERFORMANCE OF FAST RUNNING HORIZONTAL AXIS WIND TURBINE TO REACHING THE OPTIMUM DESIGN
Authors: Nazar Muneam Mahmood
Keywords: Wind Rotor, Wind Turbine, Fast Running HAWT, Optimum Design, Performance Prediction Method, NACA 4415
Issue Date: 1-Jun-2011
Publisher: University of Diyala – College of Engineering
Citation: https://djes.info/index.php/djes/article/view/589
Abstract: A computer program in visual basic was designed to predict the performance of fast running horizontal axis wind turbine for electricity generation by using blade element theory and momentum theory. NACA 4415 was chosen for the aerofoil section of blade. the design parameters ( design tip speed ratio , rotor radius and blade number ) represented in scroll bars was designed in visual basic, and by changing these parameters , solidity, chord line and twist angle curves along the blade, in addition to the rotor performance curve (relation of power coefficient with tip speed ratio), will be draw instantly. The numerical integration (trapezoidal method) was used to compute the area under rotor performance curve, the program will record the value of this area, and by change parameter design and by knowing the maximum value of area, we will know the optimal design for turbine rotor. The three and four rotor blades and the values of design tip speed ratio between (5 - 9) give the best performance of rotor. The effect change of rotor radius on performance rotor was found very small, and there is no noticed effect to rated wind speed on rotor performance when changing parameter design in computer program
URI: http://148.72.244.84:8080/xmlui/handle/xmlui/13125
ISSN: 1999-8716
Appears in Collections:مجلة ديالى للعلوم الهندسية / Diyala Journal of Engineering Sciences (DJES)

Files in This Item:
File Description SizeFormat 
البحث الخامس م.pdf1.22 MBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.