A combustion instability in a combustor terminated by a nozzle is analysed and modelled
based on a low-order Helmholtz solver. A large eddy simulation (LES) of the corresponding …

The present study is focused on the analysis of non-premixed combustion in high-velocity
(supersonic) flows. The computations make use of a large eddy simulation (LES) model …

This work explores the use of surface-mesh flow solvers to model solid rocket internal
ballistics with arbitrary grain geometry. Specifically, a surface-vorticity approach, originally …

Reactive and nonreactive Reynolds-averaged Navier–Stokes simulations of hydrogen
injection into a confined transverse supersonic flow of vitiated air are conducted. The …

The description of combustion in high-speed turbulent flows, where turbulent mixing,
compressibility effects, and chemical kinetics processes are competing, still remains a …

The triggering combustion instability in the solid rocket motor is investigated from a
nonlinear dynamical system perspective. A coupling model taking both the nonlinear …

In this work, a compressible biglobal stability approach is used to investigate the growth
characteristics of hydrodynamic and vorticoacoustic waves in porous tubes with uniform wall …

The present article aims at enhancing the computation of the global stability modes of the
internal flow of solid rocket motors (SRMs) approximated by the Taylor–Culick solution. This …

This work relies on a compressible biglobal stability approach to describe the wave
dynamics in a planar rocket chamber modeled as a porous channel. At first, the …

The combustion of composite solid propellants shows velocity fluctuations which are
expected to have marked effects on turbulence or aeroacoustic instabilities. In this work, we …