Engineering topics
Lemcherfi, Aaron I.
Publications and source records attributed to Lemcherfi, Aaron I..
Performance Characterization of a Natural Gas-Air Rotating Detonation Engine at Elevated Pressure
Performance of a rotating detonation engine was studied to understand the challenges of achieving and quantifying a net pressure gain at engine-relevant conditions. The combustor under study was designed for operation with natural gas and air at elevated chamber pressures and air preheat temperatures representative of land based power generation gas turbine engines. The thrust produced by the combustor was measured to characterize its performance while high-frequency pressure transducers and high speed imaging of broadband combustion chemiluminescence provided information about the wave structure and dynamics. The rotating detonation engine was tested with two injector configurations to explore the effect of injector design and combustor operating mode on device performance. Analysis using multiple metrics showed nearly identical performance between similar operating conditions that alternately produced a single detonation wave or two counter-propagating waves in the combustion chamber. Across the range of tested conditions, a maximum pressure gain of -42% was measured. Several tests were observed to produce up to 10% more thrust than an ideal, constant pressure combustor, though this comparison ignores injection losses. Comparison of measured pressure gain with idealized simulations showed that the net pressure gain of a rotating detonation engine is closely tied to the area ratio between the inlet and outlet of the combustor.