Some aspects of the aerodynamics of Gurney flaps on a double-element wing
Some aspects of the aerodynamics of Gurney flaps on a double-element wing
Gurney flaps of different heights have been fitted to a generic double-element wing, and the effects at two typical flap angles have been observed using force and pressure measurements, and by performing flow surveys using Laser Doppler Anemometry. At a low flap setting angle of 20 deg the suction-surface flow remains attached to the trailing edge of the flap, and vortex flow features and perturbation velocities are all similar to those observed when Gurney flaps are fitted to single element wings. At a high flap deflection of 50 deg there is an extensive region of separated flow over the flap, yet the Gurney flap still alters the flow structure. The measurements suggest that the wake flow behind the Gurney flap consists of a von Karman vortex street of alternately shed vortices. The effects of the Gurney flap on the lift, zero-lift drag, and pressure distributions are reported, and the differences between the trends observed for single-element wings are discussed.
99-104
Jeffrey, David
ac4eda1d-6475-496d-b4f5-cf166ee5cb17
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Hurst, David W.
4b73ad26-ed50-4d2b-bd70-7e8f5bd8ecf6
2001
Jeffrey, David
ac4eda1d-6475-496d-b4f5-cf166ee5cb17
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Hurst, David W.
4b73ad26-ed50-4d2b-bd70-7e8f5bd8ecf6
Jeffrey, David, Zhang, Xin and Hurst, David W.
(2001)
Some aspects of the aerodynamics of Gurney flaps on a double-element wing.
Journal Fluids Engineering: Transactions of the ASME, 123 (1), .
(doi:10.1115/1.1334376).
Abstract
Gurney flaps of different heights have been fitted to a generic double-element wing, and the effects at two typical flap angles have been observed using force and pressure measurements, and by performing flow surveys using Laser Doppler Anemometry. At a low flap setting angle of 20 deg the suction-surface flow remains attached to the trailing edge of the flap, and vortex flow features and perturbation velocities are all similar to those observed when Gurney flaps are fitted to single element wings. At a high flap deflection of 50 deg there is an extensive region of separated flow over the flap, yet the Gurney flap still alters the flow structure. The measurements suggest that the wake flow behind the Gurney flap consists of a von Karman vortex street of alternately shed vortices. The effects of the Gurney flap on the lift, zero-lift drag, and pressure distributions are reported, and the differences between the trends observed for single-element wings are discussed.
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Published date: 2001
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Local EPrints ID: 21756
URI: http://eprints.soton.ac.uk/id/eprint/21756
PURE UUID: adeee6a1-6f66-402c-9602-0b0f1836345e
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Date deposited: 15 Mar 2006
Last modified: 15 Mar 2024 06:32
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Author:
David Jeffrey
Author:
Xin Zhang
Author:
David W. Hurst
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