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Aerodynamic analysis of a propeller ...

Lachowski, Felipe Ferreira.

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Aerodynamic analysis of a propeller in a turbulent boundary layer flow.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Aerodynamic analysis of a propeller in a turbulent boundary layer flow./
Author:	Lachowski, Felipe Ferreira.
Description:	193 p.
Notes:	Source: Masters Abstracts International, Volume: 52-01.
Contained By:	Masters Abstracts International52-01(E).
Subject:	Mechanical engineering. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1523427
ISBN:	9781303226977

Aerodynamic analysis of a propeller in a turbulent boundary layer flow.
Lachowski, Felipe Ferreira.

Aerodynamic analysis of a propeller in a turbulent boundary layer flow. - 193 p.

Source: Masters Abstracts International, Volume: 52-01.

Thesis (M.S.)--Florida Atlantic University, 2013.

Simulating the exact chaotic turbulent flow field about any geometry is a dilemma between accuracy and computational resources, which has been continuously studied for just over a hundred years. This thesis is a complete walk-through of the entire process utilized to approximate the flow ingested by a Sevik-type rotor based on solutions to the Reynolds Averaged Navier-Stokes equations (RANS). The Multiple Reference Frame fluid model is utilized by the code of ANSYS--FLUENT and results are validated by experimental wake data. Three open rotor configurations are studied including a uniform inflow and the rotor near a plate with and without a thick boundary layer. Furthermore, observations are made to determine the variation in velocity profiles of the ingested turbulent flow due to varying flow conditions.

ISBN: 9781303226977Subjects--Topical Terms:

649730
Mechanical engineering.

Aerodynamic analysis of a propeller in a turbulent boundary layer flow.
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008 170521s2013 ||||||||||||||||| ||eng d
020 $a 9781303226977
035 $a (MiAaPQ)AAI1523427
035 $a AAI1523427
040 $a MiAaPQ $c MiAaPQ
100 1 $a Lachowski, Felipe Ferreira. $3 3184791
245 1 0 $a Aerodynamic analysis of a propeller in a turbulent boundary layer flow.
300 $a 193 p.
500 $a Source: Masters Abstracts International, Volume: 52-01.
500 $a Adviser: Stewart Glegg.
502 $a Thesis (M.S.)--Florida Atlantic University, 2013.
520 $a Simulating the exact chaotic turbulent flow field about any geometry is a dilemma between accuracy and computational resources, which has been continuously studied for just over a hundred years. This thesis is a complete walk-through of the entire process utilized to approximate the flow ingested by a Sevik-type rotor based on solutions to the Reynolds Averaged Navier-Stokes equations (RANS). The Multiple Reference Frame fluid model is utilized by the code of ANSYS--FLUENT and results are validated by experimental wake data. Three open rotor configurations are studied including a uniform inflow and the rotor near a plate with and without a thick boundary layer. Furthermore, observations are made to determine the variation in velocity profiles of the ingested turbulent flow due to varying flow conditions.
590 $a School code: 0119.
650 4 $a Mechanical engineering. $3 649730
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Ocean engineering. $3 660731
690 $a 0548
690 $a 0538
690 $a 0547
710 2 $a Florida Atlantic University. $b Ocean and Mechanical Engineering. $3 3175699
773 0 $t Masters Abstracts International $g 52-01(E).
790 $a 0119
791 $a M.S.
792 $a 2013
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1523427