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Journal ArticleDOI

Vortex Asymmetry and Induced Side Forces on Elliptic Cones at High Incidence

P. R. Viswanath
- 01 Sep 1995 - 
- Vol. 32, Iss: 5, pp 1018-1025
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TLDR
In this article, the authors investigated features of vortex asymmetry and induced side forces on a family of three elliptic cones at subsonic speeds, and found that ellipticity progressively reduces the angle of attack for the onset of side force up to an ellipticity ratio (defined here as the ratio of major to minor axis) of 143.
Abstract
Experimental studies were carried out investigating features of vortex asymmetry and induced side forces on a family of three elliptic cones at subsonic speeds Measurements of forces, moments, and surface flow visualization studies were made up to an angle of attack of 45 deg over a wide range of Reynolds number Results show that ellipticity progressively reduces the angle of attack for the onset of side force up to an ellipticity ratio (defined here as the ratio of major to minor axis) of 143, beyond which there is a reversal in this trend for both horizontal as well as vertical orientations of the ellipse Interestingly, the (maximum) side force magnitudes are larger for the horizontal compared to the vertical ellipse orientation on each model A correlation of the angle of attack for the onset of asymmetry on pointed forebodies with elliptic cross section is suggested These results provide strong support to the hypothesis (often made in the literature) that inviscid mechanisms may play a key role in triggering asymmetry of vortex flows

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Citations
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Journal ArticleDOI

Nose Bluntness for Side-Force Control on Circular Cones at High Incidence

TL;DR: In this paper, the effect of nose bluntness on the characteristics of vortex asymmetry and induced side forces on slender cone models at low speeds was investigated, and the results showed that the onset of vortex-asymmetry with nose blunting correlates with geometrical parameters and is practically independent of Reynolds number.
Proceedings ArticleDOI

Plasma control of forebody nose vortex symmetry breaking

TL;DR: In this article, the stability of the separation saddle point at the origin of the feeding sheet in the cross flow plane is assessed and a discrete point vortex model and slender body theory are used to identify key dimensionless parameters and model the basic physics.
Journal ArticleDOI

Forebody Geometry Effects on the Flow of a Blunt-Nose Projectile at High Alpha

TL;DR: In this article, the effect of nose shapes and a passive strake control device on the side force and yawing moment was examined on a projectile at high incidence, and it was found that the elliptical nose results in flow behaviors typical of a blunt nose, whereas the hemispheric nose resulted in behaviors that are akin to a pointed nose.
Journal ArticleDOI

Nose Blowing for Side Force Control on Slender Cones at High Incidence

TL;DR: In this article, an experimental investigation has been carried out at low speeds to study the effectiveness of axial nose blowing against the oncoming flow for side force control on two slender cones.
Journal ArticleDOI

Influence of propeller slipstream on vortex flow field over a typical micro air vehicle

TL;DR: In this article, the effect of propeller-induced slipstream on the vortex flow field on a fixed-wing Micro Air Vehicle (MAV) was explored at a freestream velocity of 10 m/s.
References
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Proceedings ArticleDOI

Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack

TL;DR: In this paper, the authors presented results from extensive wind-tunnel tests that include variations in axial and cross-sectional shape, fineness ratio, bluntness, strakes, and boundary-layer trips over a wide range of conditions (angles of attack to 90 degrees, angles of sideslip to 30 degrees, Reynolds numbers from subcritical to supercritical, and Mach numbers from 0.1 to 0.7).
Journal ArticleDOI

Numerical simulation of the effect of spatial disturbances on vortex asymmetry

TL;DR: In this paper, the steady asymmetric vortex pattern observed on slender bodies of revolution at large angle of attack was investigated using fine-grid Navier-Stokes computations and the computed results demonstrate the marked asymmetry which has been observed in experiments.
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