50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
DOI: 10.2514/6.2014-3774
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Stability Characterization of a High Pressure Transverse Combustor with Discretely Variable Oxidizer Post Lengths

Abstract: A two-dimensional chamber containing seven ox-centered shear coaxial injector elements was designed to generate and modulate an unsteady transverse flowfield. A single Study element was placed in the middle of this unsteady flowfield so its response can be measured using pressure measurement and high speed imagery. The initial characterization of this combustor entailed the effect of post length configurations on pressure amplitude. With all other conditions held constant, a long oxidizer post configuration wa… Show more

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