Control of flow separation from leading edge of a shallow rectangular cylinder through momentum injection

Finding a method to suppress aeroelastic vibrations of a bridge deck is an important research to construct a superlong suspension bridge with the main span longer than 2000 m. For this end, the boundary-layer control method was proposed and a fundamental experimental research was conducted. This met...

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Veröffentlicht in:Journal of wind engineering and industrial aerodynamics 1999, Vol.83 (1), p.503-514
Hauptverfasser: Kubo, Yoshinobu, Yukoku, Eijirou, J. Modi, Vinod, Yamaguchi, Eiki, Kato, Kusuo, Kawamura, Shin-ichi
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container_issue 1
container_start_page 503
container_title Journal of wind engineering and industrial aerodynamics
container_volume 83
creator Kubo, Yoshinobu
Yukoku, Eijirou
J. Modi, Vinod
Yamaguchi, Eiki
Kato, Kusuo
Kawamura, Shin-ichi
description Finding a method to suppress aeroelastic vibrations of a bridge deck is an important research to construct a superlong suspension bridge with the main span longer than 2000 m. For this end, the boundary-layer control method was proposed and a fundamental experimental research was conducted. This method was applied to the suppression of torsional flutter of a shallow rectangular prism which was one of typical fundamental configurations of a bridge deck section. The results obtained from measurements of surface pressure distributions and aeroelastic vibration responses showed that the proposed boundary-layer control method through momentum injection was effective for suppressing the torsional flutter of a shallow rectangular prism.
doi_str_mv 10.1016/S0167-6105(99)00097-5
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subjects Active control
Boundary layer
Boundary layer flow
Bridge decks
Cylinders (shapes)
Dynamic response
Flutter
Flutter (aerodynamics)
Pressure distribution
Rotor
Superlong span bridge
Vibration control
title Control of flow separation from leading edge of a shallow rectangular cylinder through momentum injection
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