The objective of this study was to measure the response of a gas-gas injector to velocity perturbations through CH* emission intensity at a range of instability levels and to provide quality data for comparison with high-fidelity models. To achieve this, an optically accessible, 2-D combustion chamber which self-excites a transverse instability was modified to incorporate a gas-gas shear coaxial injector at the location which coincides with the 1W velocity anti-node in the chamber. By changing the driving injector orientation, different levels of instability were produced, ranging from 8% to 65% of the mean chamber pressure. Filtered high speed video was used to measure CH* chemiluminescence, which was used to provide insight into the coupl...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
The purpose of this project was to investigate the effects of optical absorption on line-of-sight in...
Fluid mechanical coupling between injected reactants and the flame-base is observed in a gas turbine...
This research aimed to gain a better understanding of the response of a gas-centered swirl coaxial i...
An experimental rocket combustor was designed and tested to investigate the effects of injector elem...
A two dimensional transverse combustor capable of producing and modulating an unstable flowfield was...
Combustion instability in rocket engines has been a significant problem that has been studied for de...
Gaseous methane and 90% hydrogen peroxide at an equivalence ratio of 0.8 were used to study combusti...
The objective of this paper is to observe the effects of injection conditions on flame structures in...
The continued advancement of gas turbine combustion technology for power generation and propulsion a...
The continued advancement of gas turbine combustion technology for power generation and propulsion a...
Concurrent simulations and experiments are used to study combustion instabilities in a multiple inje...
The measurement of the heat release is a key part of characterizing the combusti...
The measurement of the heat release is a key part of characterizing the combusti...
Improving fidelity in simulation of combustion dynamics in rocket combustors requires an increase in...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
The purpose of this project was to investigate the effects of optical absorption on line-of-sight in...
Fluid mechanical coupling between injected reactants and the flame-base is observed in a gas turbine...
This research aimed to gain a better understanding of the response of a gas-centered swirl coaxial i...
An experimental rocket combustor was designed and tested to investigate the effects of injector elem...
A two dimensional transverse combustor capable of producing and modulating an unstable flowfield was...
Combustion instability in rocket engines has been a significant problem that has been studied for de...
Gaseous methane and 90% hydrogen peroxide at an equivalence ratio of 0.8 were used to study combusti...
The objective of this paper is to observe the effects of injection conditions on flame structures in...
The continued advancement of gas turbine combustion technology for power generation and propulsion a...
The continued advancement of gas turbine combustion technology for power generation and propulsion a...
Concurrent simulations and experiments are used to study combustion instabilities in a multiple inje...
The measurement of the heat release is a key part of characterizing the combusti...
The measurement of the heat release is a key part of characterizing the combusti...
Improving fidelity in simulation of combustion dynamics in rocket combustors requires an increase in...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
The purpose of this project was to investigate the effects of optical absorption on line-of-sight in...
Fluid mechanical coupling between injected reactants and the flame-base is observed in a gas turbine...