Advances in global linear instability analysis of nonparallel and three-dimensional flows
V Theofilis - Progress in aerospace sciences, 2003 - Elsevier
A summary is presented of physical insights gained into three-dimensional linear instability
through solution of the two-dimensional partial-differential-equation-based nonsymmetric …
through solution of the two-dimensional partial-differential-equation-based nonsymmetric …
Spike-type compressor stall inception, detection, and control
CS Tan, I Day, S Morris, A Wadia - Annual review of fluid …, 2010 - annualreviews.org
An aerodynamic instability known as stall occurs in axial compressors as the mass flow rate
is reduced and the blade loading reaches its limit. At this limiting condition, an easily …
is reduced and the blade loading reaches its limit. At this limiting condition, an easily …
Wake vortex characteristics of transport aircraft
C Breitsamter - Progress in Aerospace Sciences, 2011 - Elsevier
The flow and flight physics of wake vortex systems has been intensively investigated
concentrating on a large variety of aspects. This paper gives a brief overview on past and …
concentrating on a large variety of aspects. This paper gives a brief overview on past and …
Miniaturization of laser doppler vibrometers—a review
Laser Doppler vibrometry (LDV) is a non-contact vibration measurement technique based
on the Doppler effect of the reflected laser beam. Thanks to its feature of high resolution and …
on the Doppler effect of the reflected laser beam. Thanks to its feature of high resolution and …
Viscous linear stability analysis of rectangular duct and cavity flows
V Theofilis, PW Duck, J Owen - Journal of Fluid Mechanics, 2004 - cambridge.org
The viscous linear stability of four classes of incompressible flows inside rectangular
containers is studied numerically. In the first class the instability of flow through a rectangular …
containers is studied numerically. In the first class the instability of flow through a rectangular …
Kelvin waves and the singular modes of the Lamb–Oseen vortex
Columnar vortices are known to support a family of waves initially discovered by Lord Kelvin
(1880) in the case of the Rankine vortex model. This paper presents an exhaustive …
(1880) in the case of the Rankine vortex model. This paper presents an exhaustive …
Viscous instabilities in trailing vortices at large swirl numbers
Viscous instabilities in trailing vortices at large swirl numbers Page 1 J. Fluid Mech. (2004), vol.
500, pp. 239–262. c 2004 Cambridge University Press DOI: 10.1017/S0022112003007353 …
500, pp. 239–262. c 2004 Cambridge University Press DOI: 10.1017/S0022112003007353 …
Vortex methods and their application to trailing wake vortex simulations
G Winckelmans, R Cocle, L Dufresne… - Comptes Rendus Physique, 2005 - Elsevier
Vortex methods are competitive for simulating incompressible unsteady flows, because they
have negligible dispersion error and good energy conservation. The various methods are …
have negligible dispersion error and good energy conservation. The various methods are …
Accelerated decay of a Lamb–Oseen vortex tube laden with inertial particles in Eulerian–Lagrangian simulations
S Shuai, MH Kasbaoui - journal of fluid mechanics, 2022 - cambridge.org
We investigate the effect of inertial particles on the stability and decay of a prototypical vortex
tube, represented by a two-dimensional Lamb–Oseen vortex. In the absence of particles, the …
tube, represented by a two-dimensional Lamb–Oseen vortex. In the absence of particles, the …
On the effect of active flow control on the meandering of a wing-tip vortex
M Dghim, M Ferchichi, H Fellouah - Journal of Fluid Mechanics, 2020 - cambridge.org
The development of a wing-tip vortex of a rectangular, square-tipped wing having a NACA
0012 airfoil at a chord Reynolds number. Under the most effective configuration, case C3 …
0012 airfoil at a chord Reynolds number. Under the most effective configuration, case C3 …