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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
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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Taylor-Görtler Vortices in the Flow Driven by a Rotating Magnetic Field in a Cylindrical Container

TL;DR: A study of various methods for identifying vortex cores, including the so-called λ2 and Qriteria, which found the Q criterion proved particularly useful when applied to the fluctuation velocity field.
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Classification of turbulent flow patterns with fuzzy clustering

TL;DR: A pattern recognition technique for the identification of critical points in turbulent flows based on fuzzy C-means clustering was applied to hot-wire data from two different turbulent flows; one is the highly ordered wake of a mesh strip, while the second is thewake of a circular cylinder, which has a higher level of disorder.
Journal ArticleDOI

Behaviour of small-scale turbulence in the turbulent/non-turbulent interface region of developing turbulent jets

TL;DR: Breda et al. as mentioned in this paper examined the modification of the turbulent/non-turbulent interface (TNTI) and spatial evolution of the small-scale behavior of these different jets, which are both important factors behind determining the entrainment rate.
Journal ArticleDOI

Flow structures govern particle collisions in turbulence

TL;DR: In this paper, direct numerical simulations find that rapid head-on collisions of particles mostly occur in regions of straining compared to vortical regions, and that intense vortex tubes conspire with enveloping straining sheets, in the form of vortex-strain worm-rolls, to generate violent collisions.
Journal ArticleDOI

Simulation and modelling of a skewed turbulent channel flow

TL;DR: In this article, a time-dependent three-dimensionalally skewed flow is investigated using direct numerical simulations of the incompressible Navier-Stokes equations, and the effect on the instantaneous and mean turbulent field is investigated.
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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