SIMULATION AND MODELING OF AN ACOUSTICALLY FORCED MODEL ROCKET INJECTOR
dc.contributor.advisor | Yu, Ken | en_US |
dc.contributor.author | Gers, David | en_US |
dc.contributor.department | Aerospace Engineering | en_US |
dc.contributor.publisher | Digital Repository at the University of Maryland | en_US |
dc.contributor.publisher | University of Maryland (College Park, Md.) | en_US |
dc.date.accessioned | 2010-10-07T06:05:09Z | |
dc.date.available | 2010-10-07T06:05:09Z | |
dc.date.issued | 2010 | en_US |
dc.description.abstract | A numerical and experimental study was performed to assess the capability of the Loci-CHEM CFD solver in simulating dynamic interaction between hydrogen-oxygen turbulent diffusion flames and periodic pressure waves. Previous experimental studies involving a single-element shear-coaxial model injector revealed an unusual flame-acoustic interaction mechanism affecting combustion instability characteristics. To directly compare the simulation and experiments, various models in the present solver were examined and additional experiments conducted. A customized mesh and corresponding boundary conditions were designed and developed, closely approximating the experimental setup. Full 3-D simulations were conducted using a hybrid RANS/LES framework with appropriate chemistry and turbulence models. The results were compared for both reacting and non-reacting flows that were excited at various forcing frequencies representing both resonant and non-resonant behaviors. Although a good qualitative agreement was obtained for the most part, there was a significant discrepancy in simulating the flame-acoustic interaction behavior observed under non-resonant forcing conditions. | en_US |
dc.identifier.uri | http://hdl.handle.net/1903/10917 | |
dc.subject.pqcontrolled | Engineering, Aerospace | en_US |
dc.subject.pquncontrolled | CFD | en_US |
dc.subject.pquncontrolled | combustion instability | en_US |
dc.subject.pquncontrolled | Loci-Chem | en_US |
dc.subject.pquncontrolled | propulsion | en_US |
dc.subject.pquncontrolled | rocket engine | en_US |
dc.title | SIMULATION AND MODELING OF AN ACOUSTICALLY FORCED MODEL ROCKET INJECTOR | en_US |
dc.type | Thesis | en_US |
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