RDCs have received considerable attention, however experimental measurements of the static pressure field in the combustor are difficult. It is necessary to develop a measurement technique to preserve the sensor while providing a temporally resolved pressure. The performance of the transfer function at other frequencies/ amplitudes needs to be further quantified. The final version o f t his work will incorporate the corrected static pressure signal and averaging procedures to measure the pressure field through the combustion chamber and investigate the variation in this pressure field through the variation of key combustor parameters such as outlet restriction, mass flow rate, and equivalence ratio, among other values. field
The energy transfer from the heat release of the combustion to the acoustic pressure oscillations is...
Over the past few decades, there has been significant research into propulsion concepts attempting t...
The paper summarizes research that was conducted last year as part of the project of “Turbine engine...
RDCs have received considerable attention, however experimental measurements of the static pressure ...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...
The utility of high fidelity (HF) pressure measurements from Continuous Variable Resonance Combustor...
A Rotating Detonation Combustor (RDC) is a novel pressure gain combustion device, in which a detonat...
The utility of high fidelity (HF) pressure measurements from Continuous Variable Resonance Combustor...
A time resolved, two-dimensional reactive Euler solver is employed to simulate Rotating Detonation C...
As gas turbine combustion systems evolve to achieve ultra-low emission targets, monitoring and contr...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Lean low emission combustors are prone to combustion instabilities. Information on the impact of pre...
The energy transfer from the heat release of the combustion to the acoustic pressure oscillations is...
Over the past few decades, there has been significant research into propulsion concepts attempting t...
The paper summarizes research that was conducted last year as part of the project of “Turbine engine...
RDCs have received considerable attention, however experimental measurements of the static pressure ...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
Rotating Detonation Combustors (RDC) feature an inherently unsteady internal flow field with charact...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...
This work investigates the stagnation pressure gain in rotating detonation combustors (RDC) and its ...
The utility of high fidelity (HF) pressure measurements from Continuous Variable Resonance Combustor...
A Rotating Detonation Combustor (RDC) is a novel pressure gain combustion device, in which a detonat...
The utility of high fidelity (HF) pressure measurements from Continuous Variable Resonance Combustor...
A time resolved, two-dimensional reactive Euler solver is employed to simulate Rotating Detonation C...
As gas turbine combustion systems evolve to achieve ultra-low emission targets, monitoring and contr...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Lean low emission combustors are prone to combustion instabilities. Information on the impact of pre...
The energy transfer from the heat release of the combustion to the acoustic pressure oscillations is...
Over the past few decades, there has been significant research into propulsion concepts attempting t...
The paper summarizes research that was conducted last year as part of the project of “Turbine engine...