To investigate the effects of the nozzle-exit conditions on jet flow and sound fields, large- eddy simulations of an isothermal Mach 0.9 jet issued from a convergent-straight nozzle are …
The precessing vortex core (PVC) is a coherent flow structure that is often encountered in swirling flows in gas turbine (GT) combustors. In some swirl combustors, it has been …
The purpose of this paper is to characterize and model waves that are observed within the potential core of subsonic jets and relate them to previously observed tones in the near …
K Gudmundsson, T Colonius - Journal of Fluid Mechanics, 2011 - cambridge.org
Previous work has shown that aspects of the evolution of large-scale structures, particularly in forced and transitional mixing layers and jets, can be described by linear and nonlinear …
Coherent turbulent wave-packet structures in a jet at Reynolds number 460 000 and Mach number 0.4 are extracted from experimental measurements and are modeled as linear …
This paper explores the screech closure mechanism for different axisymmetric modes in shock-containing jets. While many of the discontinuities in tonal frequency exhibited by …
Streaks have been found to be an important part of wall-turbulence dynamics. In this paper, we extend the analysis for unbounded shear flows, in particular a Mach 0.4 round jet, using …
We model the resonance mechanism underpinning generation of A1 and A2 screech tones in an under-expanded supersonic jet. Starting from the resonance model recently proposed …
We present an analysis of the linear stability characteristics of shock-containing jets. The flow is linearised around a spatially periodic mean, which acts as a surrogate for a mean …