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Journal ArticleDOI

A general classification of three-dimensional flow fields

Min S Chong, +2 more
- 01 May 1990 - 
- Vol. 2, Iss: 5, pp 765-777
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TLDR
In this paper, the geometry of solution trajectories for three first-order coupled linear differential equations can be related and classified using three matrix invariants for elementary three-dimensional flow patterns defined by instantaneous streamlines for flow at and away from no slip boundaries for both compressible and incompressible flow.
Abstract
The geometry of solution trajectories for three first‐order coupled linear differential equations can be related and classified using three matrix invariants. This provides a generalized approach to the classification of elementary three‐dimensional flow patterns defined by instantaneous streamlines for flow at and away from no‐slip boundaries for both compressible and incompressible flow. Although the attention of this paper is on the velocity field and its associated deformation tensor, the results are valid for any smooth three‐dimensional vector field. For example, there may be situations where it is appropriate to work in terms of the vorticity field or pressure gradient field. In any case, it is expected that the results presented here will be of use in the interpretation of complex flow field data.

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Citations
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Experimental analysis of the aero-acoustic coupling in a plane impinging jet on a slotted plate

TL;DR: In this paper, a plane jet issuing from a rectangular nozzle and impinging on a plate is considered for Re ǫ = 3900, and the sound pressure, the vibration of the impinged plate and the spatial velocity field are obtained simultaneously using a microphone, an accelerometer and the time-resolved particle image velocimetry technique, respectively.
Journal ArticleDOI

Volume reconstruction of an impinging jet obtained from stereoscopic-PIV data using POD

TL;DR: In this article, an experimental platform has been developed to generate a flow at different Reynolds numbers and the dynamics of these flows are investigated experimentally using the stereoscopic PIV technique, where the kinematic fields of parallel planes are measured by SPIV acquisitions in order to study the corresponding fluid flow.

Extraction of Vortex Structures in 3D Flow Fields

Jan Sahner
TL;DR: This thesis presents a novel extraction approach for swirling stream line motion cores in snapshots of the flow field and demonstrates how those structures can be tracked in time by appropriate feature flow fields, and develops the first derivative free feature line extraction method for surface meshes.
Journal ArticleDOI

Is vortex stretching the main cause of the turbulent energy cascade

TL;DR: In this paper, the authors derived a new result for the average flux of kinetic energy between two points in the flow that reveals the role of vortex stretching and showed that vortex stretching is in fact not the main contributor to the average energy cascade; the main contribution is the self-amplification of the strain-rate field.
Journal ArticleDOI

Flow structure around a low-drag Ahmed body

TL;DR: In this paper, a conceptual flow structure model is proposed for a low-drag Ahmed body, including both steady and unsteady coherent structures around the body, and a corner vortex is observed near the lower end of the slanted surface.
References
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Book

Nonlinear Oscillations, Dynamical Systems, and Bifurcations of Vector Fields

TL;DR: In this article, the authors introduce differential equations and dynamical systems, including hyperbolic sets, Sympolic Dynamics, and Strange Attractors, and global bifurcations.

A Reflection on Nonlinear Oscillations, Dynamical Systems, and Bifurcations of Vector Fields

TL;DR: In this paper, the authors introduce differential equations and dynamical systems, including hyperbolic sets, Sympolic Dynamics, and Strange Attractors, and global bifurcations.
Book

Differential Equations, Dynamical Systems, and Linear Algebra

TL;DR: In this article, the structure theory of linear operators on finite-dimensional vector spaces has been studied and a self-contained treatment of that subject is given, along with a discussion of the relations between dynamical systems and certain fields outside pure mathematics.
Journal ArticleDOI

Direct simulation of a turbulent boundary layer up to R sub theta = 1410

TL;DR: In this paper, the turbulent boundary layer on a flat plate, with zero pressure gradient, is simulated numerically at four stations between R sub theta = 225 and R sub tta = 1410.
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