Computational Optimization of a Rotary Valved Pulse Combustor Concept

Daniel E Paxson; H Douglas Perkins; Shaye Yungster

NASA NTRS · 20240014883

Computational Optimization of a Rotary Valved Pulse Combustor Concept

Daniel E Paxson·H Douglas Perkins·Shaye Yungster

Abstract

A resonant pulse combustor valve concept is introduced that utilizes two slotted, coaxial counterrotating discs for mechanical actuation at the combustor inlet. The intended test article for prototype demonstration is a small, 22 in. long, propane fueled laboratory combustor, flowing approximately 0.006 lbm/s of air. The objective is to develop an externally actuated (i.e., active) valve that yields better performance and longer life than the traditional internally actuated (i.e., passive), reed-type valve found on most pulse combustors. The rotary valve motion is optimized using an axisymmetric, two-dimensional computational fluid dynamic simulation with a domain that includes the valve as a moveable interior wall. Parameters such as slew rate, dwell period in the open position, and total closed period are varied using fuel specific impulse as the figure of merit. Variations in fuel injector location and air fuel ratio are also examined. Additionally, the performance impact of leakage from the rotary valve is quantified since leakage is endemic to the design. The optimized simulation results indicate that the rotary valve concept can deliver the desired performance attributes using disc rotational speeds and stresses that are well within the realm of modern materials. A preliminary mechanical valve design is included in the report.

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Daniel E Paxson, H Douglas Perkins, Shaye Yungster. Computational Optimization of a Rotary Valved Pulse Combustor Concept. https://ntrs.nasa.gov/citations/20240014883

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