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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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Proceedings ArticleDOI

Structure of vortex breakdown on a pitching delta wing

Miguel Visbal
TL;DR: In this paper, an analysis of the dynamics of vortex breakdown is presented, and a description of the 3D instantaneous structure of the flow field is provided for the first time using critical-point theory.
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Enstrophy transport conditional on local flow topologies in different regimes of premixed turbulent combustion

TL;DR: The interrelation between the enstrophy transport and flow topologies, which can be assigned to eight categories based on the three invariants of the velocity-gradient tensor, has been analysed here.
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Decrement of spanwise vortices by a drag-reducing riblet surface

TL;DR: In this article, the spanwise vortices in a turbulent flow over drag-reducing V-shaped riblet grooves have been investigated experimentally, and the number distributions of the vortex cores were analyzed statistically.
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Effects of leading edge geometry on the vortex shedding frequency of an elongated bluff body at high Reynolds numbers

TL;DR: In this article, a large scale wind tunnel on an elongated bluff body with a chord-to-thickness ratio of 7 over the Reynolds number range Re=4.0-7.5×10 4.
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Multiscale analysis of the invariants of the velocity gradient tensor in isotropic turbulence

TL;DR: In this article, a detailed study on the scale dependence of various quantities of interest, such as the population fraction of different flow-topologies, is presented, while the quantities appear close to scale invariant in inertial range, a ''bump'' is observed at length scales between the inertial and viscous ranges.
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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