The longitudinal combustion instability characteristics of a pintle injector for a liquid rocket
engine combustor are investigated experimentally. The effects of the propellant total …

Axisymmetric simulations of a liquid rocket engine are performed using a delayed detached-
eddy-simulation (DDES) turbulence model with the Compressible Flamelet Progress …

Combustion instability is investigated computationally for a ten-injector rocket engine using
a compressible flamelet progress variable (FPV) model and detached eddy simulation …

Although the transported probability density function (PDF) method has been developed for
decades, its application has been mainly focused on the low-Mach number flow problems …

Combustion instability resulting from thermo-acoustic interaction is a serious issue in
highpower, high-energy density propulsion devices like rocket engines, gas turbines and …

This paper invokes a reactive flow large eddy simulation (LES) framework to simulate
combustion instabilities in a sub-scale rocket combustion chamber. A model rocket …

Combustion driven thermo-acoustic instability is a critical issue in the development of high-
speed propulsion devices like gas turbines, rocket engines, ramjets and scramjets which …

Combustion instability due to thermo-acoustic interactions in high-speed propulsion devices
such as gas turbines and rocket engines result from pressure waves with very large …

Although current augmented, virtual, and mixed reality (AR/VR/MR) systems are facing
advanced and immersive experience in the entertainment industry with countless media …