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dc.contributor.advisorSchobeiri, M T.
dc.creatorSharma, Kapil
dc.date.accessioned2011-08-08T22:48:28Z
dc.date.accessioned2011-08-09T01:32:38Z
dc.date.available2011-08-08T22:48:28Z
dc.date.available2011-08-09T01:32:38Z
dc.date.created2011-05
dc.date.issued2011-08-08
dc.date.submittedMay 2011
dc.identifier.urihttp://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9090
dc.description.abstractThe existing 3-stage research turbine at Turbomachinery Performance and Flow Research Laboratory (TPFL) facility, Texas A & M University (TAMU) was replaced with a newly designed and manufactured 2-stage turbine in accordance with the design requirements as per DooSan, DHI. This new design of turbine consisted of bowed stator and rotor blades to study the effect on reduction of secondary ow losses and thus improvement in turbine efficiency if any. The new design also incorporated labyrinth seals on both inner and outer shrouds. Extensive Inter-stage and Performance experiments were carried out on this new turbine. Inter-stage measurements were accomplished by traversing three 5-hole probes radially and circumferentially, using the existing probe traverse system in TPFL. Performance tests were conducted for varying pressure ratio, at fixed rotational speed and for varying rotational speed with fixed pressure ratio and the efficiency was plotted against u/c_0. Each condition was tested and measured two to three times to check for reproducibility of the data. The results from inter-stage experiments show that the rotor row loss coefficient is about four times higher than the stator row loss coefficient. This high rotor loss coefficient reduces the total to static efficiency. From the performance tests, the maximum total-to-static efficiency observed was 85.2 percent located at around u/c_0 = 0.75. This relatively low efficiency is in consonance with the inter-stage results (high rotor loss coefficient).en
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.subject2-stage turbineen
dc.subjectrotor bladesen
dc.subjectbowed statoren
dc.titleInter-stage and Performance Tests of a Two-stage High-pressure Turbineen
dc.typeThesisen
thesis.degree.departmentMechanical Engineeringen
thesis.degree.disciplineMechanical Engineeringen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameMaster of Scienceen
thesis.degree.levelMastersen
dc.contributor.committeeMemberHan, J C.
dc.contributor.committeeMemberHassan, Y A.
dc.type.genrethesisen
dc.type.materialtexten


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