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Improving the Performance of an Active Valve Resonant Pulse Combustor
Author(s) -
Joel C. Lisanti,
Xuren Zhu,
William L. Roberts
Publication year - 2019
Publication title -
aiaa propulsion and energy 2020 forum
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2019-3871
Subject(s) - combustor , materials science , pulse (music) , electrical engineering , optoelectronics , engineering , combustion , voltage , chemistry , organic chemistry
The following study describes an experimental investigation into the key parameters influencing the performance and operation of an actively driven resonant pulse combustor. The experimental apparatus is composed of a rotary valved pulse combustor with modular components, including the capability ofmodifying the convective distance between the active valve and fuel injection. The performance was characterized through pitot probe measurement of the averaged stagnation pressure at the combustor exit, measurement of the dynamic combustion chamber pressure, and recording of an ion probe signal to indicate heat release timing. Results demonstrate that small changes in relevant characteristic time scales (i.e. inlet air convection time) can have a meaningful impact on the device operation and performance. This suggests that moderate design optimization may result in a significant performance improvements.

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