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TRANSIENT TEMPERATURE MEASUREMENTS OF COMBUSTOR WALLS ENCLOSING A 2-D MODEL COAXIAL INJECTOR

dc.contributor.advisorYu, Kenneth Hen_US
dc.contributor.authorLee, Hak Seungen_US
dc.date.accessioned2014-02-06T06:32:20Z
dc.date.available2014-02-06T06:32:20Z
dc.date.issued2013en_US
dc.identifier.urihttp://hdl.handle.net/1903/14853
dc.description.abstractDirect measurements of combustor inner wall temperatures are difficult due to harsh flow conditions. A novel approach was used to obtain the combustor wall temperature as a function of time and location in a H2-O2 model injector, enclosing acoustically forced flames. The emphasis was to obtain thermal boundary conditions for various injector operation. The new approach combined a series of experimental measurements on the outer wall with a transient heat transfer analysis applicable for low Biot number and low Fourier number conditions. Infrared thermometry technique was applied to obtain outer wall temperature distribution at three different wall thicknesses, and these measurements were combined with the transient analysis to calibrate the amount of heat transfer and the corresponding inner wall temperature. The results showed that the combustor inner wall temperature distribution evolved much differently for acoustically forced flames, suggesting a different thermal boundary condition should be used in those cases.en_US
dc.language.isoenen_US
dc.titleTRANSIENT TEMPERATURE MEASUREMENTS OF COMBUSTOR WALLS ENCLOSING A 2-D MODEL COAXIAL INJECTORen_US
dc.typeThesisen_US
dc.contributor.publisherDigital Repository at the University of Marylanden_US
dc.contributor.publisherUniversity of Maryland (College Park, Md.)en_US
dc.contributor.departmentAerospace Engineeringen_US
dc.subject.pqcontrolledAerospace engineeringen_US
dc.subject.pquncontrolledHeat transferen_US
dc.subject.pquncontrolledInner wall temperature measurementen_US
dc.subject.pquncontrolledIR thermographyen_US
dc.subject.pquncontrolledLiquid rocketen_US
dc.subject.pquncontrolledshear coaxial injectoren_US


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