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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.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Aerodynamic analysis of a propeller in a turbulent boundary layer flow./
作者:	Lachowski, Felipe Ferreira.
面頁冊數:	193 p.
附註:	Source: Masters Abstracts International, Volume: 52-01.
Contained By:	Masters Abstracts International52-01(E).
標題:	Mechanical engineering. -
電子資源:	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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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.
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