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Design optimization of a wind turbin...

The University of Texas at Arlington.

Design optimization of a wind turbine blade.

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Design optimization of a wind turbine blade./
作者:	Koratagere Srinivasa Raju, Bharath.
面頁冊數:	84 p.
附註:	Source: Masters Abstracts International, Volume: 49-06, page: 3908.
Contained By:	Masters Abstracts International49-06.
標題:	Engineering, Aerospace. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1494380
ISBN:	9781124687421

Design optimization of a wind turbine blade.
Koratagere Srinivasa Raju, Bharath.

Design optimization of a wind turbine blade. - 84 p.

Source: Masters Abstracts International, Volume: 49-06, page: 3908.

Thesis (M.S.)--The University of Texas at Arlington, 2011.

This work focuses on designing a blade of 45 meters in length that produces a power of 1.6 MW. The design of the blade was done using the Blade Element Momentum theory and the Prandtl's tip loss factor was used. The aerodynamic loads and differential power at are tabulated and plotted.

ISBN: 9781124687421Subjects--Topical Terms:

845476
Engineering, Aerospace.

Design optimization of a wind turbine blade.
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020 $a 9781124687421
035 $a (UMI)AAI1494380
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040 $a UMI $c UMI
100 1 $a Koratagere Srinivasa Raju, Bharath. $3 845627
245 1 0 $a Design optimization of a wind turbine blade.
300 $a 84 p.
500 $a Source: Masters Abstracts International, Volume: 49-06, page: 3908.
500 $a Adviser: Bo Ping Wang.
502 $a Thesis (M.S.)--The University of Texas at Arlington, 2011.
520 $a This work focuses on designing a blade of 45 meters in length that produces a power of 1.6 MW. The design of the blade was done using the Blade Element Momentum theory and the Prandtl's tip loss factor was used. The aerodynamic loads and differential power at are tabulated and plotted.
520 $a The finite element method for analysis of the blade is used. As the chord lengths vary decreasingly along the blade radii in order to use the simple beam theory the breath and height of the blade is considered as a function of the chord length, hence the analysis is done assuming the blade to be a tapered hollow beam. The first few natural frequencies in the axial and transverse direction and mode shapes are calculated and plotted.
520 $a In order to reduce the weight of the blade designed and increase the power two sets of optimization was done. The design variables are the chord lengths, with objective function as power mass constraints was used. The other optimization was using the mass as objective function and power as the constraint. The chord distribution results are plotted and discussed.
590 $a School code: 2502.
650 4 $a Engineering, Aerospace. $3 845476
650 4 $a Energy. $3 784773
690 $a 0538
690 $a 0791
710 2 $a The University of Texas at Arlington. $b Aerospace Engineering. $3 845625
773 0 $t Masters Abstracts International $g 49-06.
790 1 0 $a Wang, Bo Ping, $e advisor
790 1 0 $a Lawrence, Kent L. $e committee member
790 1 0 $a Nomura, Seiichi $e committee member
790 $a 2502
791 $a M.S.
792 $a 2011
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1494380

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