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Parametric Study of Lift-Drag Coefficients vs. Geometric Parameters of Axial Compressor/Turbine for Flow Blade Interactions

dc.rights.licenseAll rights reserveden_US
dc.contributor.advisorRestrepo Torres, Bernardo
dc.contributor.authorGerena Colón, Diolinete del C.
dc.date.accessioned2020-10-22T14:00:14Z
dc.date.available2020-10-22T14:00:14Z
dc.date.issued2013
dc.identifier.citationGerena Colón, D. C. (2013). Parametric study of lift-drag coefficients vs. geometric parameters of axial compressor/turbine for flow blade interactions [Unpublished manuscript]. Graduate School, Polytechnic University of Puerto Rico.en_US
dc.identifier.urihttp://hdl.handle.net/20.500.12475/883
dc.descriptionDesign Project Article for the Graduate Programs at Polytechnic University of Puerto Ricoen_US
dc.description.abstractThis project is a parametric study of the Lift-Drag coefficients from blade hub to tip radius of Axial Compressor/Turbine for flow blade interactions. The study contemplates the effect of Lift and Drag forces varying the inlet blade angle and the response with an actuator Inlet Guide Vane (IGV). In the turbine section, the Lift and Drag forces are also studied varying the inlet blade angle for the rotor and the effect with different exit nozzle angles. Lift force is used to convert energy from the shaft to the fluid and vice versa while drag is the energy losses due to friction. The desired effect was found at lower inlet blade angle. The study was done using the fundamental turbomachinery equations and the compressible flow properties. KeyTerms-Axial Compressor/Turbine, Drag Coefficient, Inlet Guide Vane, Lift Coefficient, Turbomachine.en_US
dc.language.isoen_USen_US
dc.publisherPolytechnic University of Puerto Ricoen_US
dc.relation.ispartofMechanical Engineering
dc.relation.ispartofseriesSpring-2013
dc.relation.haspartSan Juanen_US
dc.subject.lcshCompressors--Bladesen_US
dc.subject.lcshAxial flow compressors--Blades
dc.subject.lcshLift (Aerodynamics)
dc.subject.lcshPolytechnic University of Puerto Rico--Graduate students--Research
dc.titleParametric Study of Lift-Drag Coefficients vs. Geometric Parameters of Axial Compressor/Turbine for Flow Blade Interactionsen_US
dc.typeArticleen_US
dc.rights.holderPolytechnic University of Puerto Rico, Graduate Schoolen_US


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