Lift Enhancement on Unconventional Airfoils

Lift augmentation on airfoils is a critical task to an aerodynamicist when asked to design new wings. Flow visualization studies on a corrugated airfoil confirm that the trapped vortices lead to a modification of the effective wing shape and an increase in lift. Considerable lift enhancement is foun...

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Main Author: Yeung, W. W. H.
Format: Conference or Workshop Item
Language:English
Published: 2006
Subjects:
Online Access:http://eprints.utm.my/316/
http://eprints.utm.my/316/1/WWH2006_LiftEnhancementonUnconventionalAirfoils.pdf
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author Yeung, W. W. H.
author_facet Yeung, W. W. H.
author_sort Yeung, W. W. H.
building UTeM Institutional Repository
collection Online Access
description Lift augmentation on airfoils is a critical task to an aerodynamicist when asked to design new wings. Flow visualization studies on a corrugated airfoil confirm that the trapped vortices lead to a modification of the effective wing shape and an increase in lift. Considerable lift enhancement is found in the experimental measurements on a wing model incorporated with a backward-facing step on the upper surface because of a trapped vortex. Furthermore, a leading-edge rotating cylinder (which behaves like a vortex) effectively extend the lift curve of an airfoil without substantially affecting its slope, thus increasing the maximum lift and delaying stall. While theoretical studies of vortex trapping are limited to airfoils with smooth surfaces, this paper explores the ability of trapping single and multiple vortices on airfoils with surface discontinuities, such as cavities, corrugations, or a rotating cylinder. Streamlines, surface pressure distributions and the vortex trajectories are presented in the hope to advance the knowledge on lift enhancement for flow past unconventional airfoils.
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spelling utm-3162017-08-23T07:37:23Z http://eprints.utm.my/316/ Lift Enhancement on Unconventional Airfoils Yeung, W. W. H. TJ Mechanical engineering and machinery TL Motor vehicles. Aeronautics. Astronautics Lift augmentation on airfoils is a critical task to an aerodynamicist when asked to design new wings. Flow visualization studies on a corrugated airfoil confirm that the trapped vortices lead to a modification of the effective wing shape and an increase in lift. Considerable lift enhancement is found in the experimental measurements on a wing model incorporated with a backward-facing step on the upper surface because of a trapped vortex. Furthermore, a leading-edge rotating cylinder (which behaves like a vortex) effectively extend the lift curve of an airfoil without substantially affecting its slope, thus increasing the maximum lift and delaying stall. While theoretical studies of vortex trapping are limited to airfoils with smooth surfaces, this paper explores the ability of trapping single and multiple vortices on airfoils with surface discontinuities, such as cavities, corrugations, or a rotating cylinder. Streamlines, surface pressure distributions and the vortex trajectories are presented in the hope to advance the knowledge on lift enhancement for flow past unconventional airfoils. 2006-07 Conference or Workshop Item PeerReviewed application/pdf en http://eprints.utm.my/316/1/WWH2006_LiftEnhancementonUnconventionalAirfoils.pdf Yeung, W. W. H. (2006) Lift Enhancement on Unconventional Airfoils. In: 1st Regional Conference on Vehicle Engineering & Technology, 3-5 July 2006, Kuala Lumpur, Malaysia.
spellingShingle TJ Mechanical engineering and machinery
TL Motor vehicles. Aeronautics. Astronautics
Yeung, W. W. H.
Lift Enhancement on Unconventional Airfoils
title Lift Enhancement on Unconventional Airfoils
title_full Lift Enhancement on Unconventional Airfoils
title_fullStr Lift Enhancement on Unconventional Airfoils
title_full_unstemmed Lift Enhancement on Unconventional Airfoils
title_short Lift Enhancement on Unconventional Airfoils
title_sort lift enhancement on unconventional airfoils
topic TJ Mechanical engineering and machinery
TL Motor vehicles. Aeronautics. Astronautics
url http://eprints.utm.my/316/
http://eprints.utm.my/316/1/WWH2006_LiftEnhancementonUnconventionalAirfoils.pdf