Separated flow around an airfoil with a spoiler

When a spoiler is erected rapidly on the upper surface of a wing, it brings about a long-term reduction in lift and an increase in drag. However, it has a transient effect of increasing the lift (usually referred to as the adverse lift) on the wing due to the creation of a starting vortex shed from...

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Main Author: Xu, Cheng.
Other Authors: Yeung, William Wai Hung
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/19974
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Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-19974
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spelling sg-ntu-dr.10356-199742023-03-11T17:24:29Z Separated flow around an airfoil with a spoiler Xu, Cheng. Yeung, William Wai Hung School of Mechanical and Production Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics When a spoiler is erected rapidly on the upper surface of a wing, it brings about a long-term reduction in lift and an increase in drag. However, it has a transient effect of increasing the lift (usually referred to as the adverse lift) on the wing due to the creation of a starting vortex shed from the tip and convected downstream of the spoiler. This thesis is devoted to a numerical study of the unsteady separated flow around an airfoil with a spoiler. Doctor of Philosophy (MPE) 2009-12-14T07:54:02Z 2009-12-14T07:54:02Z 1997 1997 Thesis http://hdl.handle.net/10356/19974 en NANYANG TECHNOLOGICAL UNIVERSITY 157 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Xu, Cheng.
Separated flow around an airfoil with a spoiler
description When a spoiler is erected rapidly on the upper surface of a wing, it brings about a long-term reduction in lift and an increase in drag. However, it has a transient effect of increasing the lift (usually referred to as the adverse lift) on the wing due to the creation of a starting vortex shed from the tip and convected downstream of the spoiler. This thesis is devoted to a numerical study of the unsteady separated flow around an airfoil with a spoiler.
author2 Yeung, William Wai Hung
author_facet Yeung, William Wai Hung
Xu, Cheng.
format Theses and Dissertations
author Xu, Cheng.
author_sort Xu, Cheng.
title Separated flow around an airfoil with a spoiler
title_short Separated flow around an airfoil with a spoiler
title_full Separated flow around an airfoil with a spoiler
title_fullStr Separated flow around an airfoil with a spoiler
title_full_unstemmed Separated flow around an airfoil with a spoiler
title_sort separated flow around an airfoil with a spoiler
publishDate 2009
url http://hdl.handle.net/10356/19974
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