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Proceedings ArticleDOI

Investigation of several passive and active methods for turbulent flow separation control

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TLDR
In this article, the relative performance of several passive and active methods for controlling two-dimensional turbulent separated flow associated with a curved backward-facing ramp was investigated at low speeds, and the results indicated that submerged vortex generators, vortex generator jets, elongated arches at +-alpha, and large-eddy breakup devices at + -alpha placed near the baseline separation location reduce flow separation and increase pressure recovery.
Abstract
Relative performance of several passive and active methods for controlling two-dimensional turbulent separated flow associated with a curved backward-facing ramp were investigated at low speeds. Surface static pressure measurement and oil flow visualization results indicate that submerged vortex generators, vortex generator jets, elongated arches at +-alpha, and large-eddy breakup devices at +-alpha placed near the baseline separation location reduce flow separation and increase pressure recovery. Spanwise cylinders reduce flow separation but decrease pressure recovery downstream. Arches with alpha = 0 deg, Helmholtz resonators, and Viets' fluidic flappers examined so far have no significant effect in reducing separation. Wall cooling computation indicates that separation delay on a partially cooled ramp is nearly the same as on a fully-cooled ramp while minimizing the frictional drag increase associated with the wall cooling process.

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Citations
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Journal ArticleDOI

Review of research on low-profile vortex generators to control boundary-layer separation

TL;DR: In this article, an in-depth review of boundary-layer flow-separation control by a passive method using low-profile vortex generators is presented, defined as those with a device height between 10% and 50% of the boundary layer thickness.
Journal ArticleDOI

Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators

TL;DR: In this article, the authors describe preliminary tests done to optimize standard passive devices before testing active systems, showing quantitatively the improvement brought by the passive devices in terms of skin friction.
Journal ArticleDOI

Streamwise vortex production by pitched and skewed jets in a turbulent boundary layer

TL;DR: Weak longitudinal vortices produced by the interaction of simple, round wall jets with a two-dimensional flow comprising a turbulent boundary layer were studied experimentally as discussed by the authors, where the jets were pitched up at 45 degrees and skewed relative to the freestream as they entered from the wall.
Journal ArticleDOI

Turbine Separation Control Using Pulsed Vortex Generator Jets

TL;DR: In this article, the application of pulsed vortex generator jets to control separation on the suction surface of a low-pressure turbine blade is reported, and the results show that the effect of the pulsed generator jets is comparable to that of steady jets with an order of magnitude less massflow.
ReportDOI

Active load control techniques for wind turbines.

TL;DR: In this paper, the authors provide an overview on the current state of wind turbine control and introduce a number of active techniques that could be potentially used for control of wind turbines blades.
References
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Journal ArticleDOI

Flow around a circular cylinder near a plane boundary

TL;DR: In this article, the authors measured the mean pressure around a circular cylinder placed at various heights above a plane boundary and found that the turbulent boundary layer on the plate at the cylinder position, but with it removed from the tunnel, was equal to 0·8 of the cylinder diameter.

Investigation of the Stability of the Laminar Boundary Layer in a Compressible Fluid

TL;DR: In this article, the stability of two-dimensional laminar flows of a gas is investigated by the method of small perturbations, and the main emphasis is placed on the case of the laminars boundary layer.
Journal ArticleDOI

Vortex shedding from a rectangular prism and a circular cylinder placed vertically in a turbulent boundary layer

TL;DR: In this article, the Strouhal number for the rectangular prism and the circular cylinder was found to be a power function of the aspect ratio h / w (or h / d ). Here f c is the vortex shedding frequency, U 0 is the free-stream velocity, h is the height, w is the width and d is the diameter.
Journal ArticleDOI

Subsonic diffusers designed integrally with vortex generators.

TL;DR: In this paper, a short subsonic diffuser incorporating vortex generators as an integral design feature was developed at Lockheed and compared experimentally with a conventional high-performance trumpet-shaped diffuser.
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