A stage-by-stage post-stall compression system modeling technique: methodology, validation, and application
dc.contributor.author | Davis, Milton W. Jr. | en |
dc.contributor.committeechair | O'Brien, Walter F. Jr. | en |
dc.contributor.committeemember | Moore, John | en |
dc.contributor.committeemember | Leonard, Robert G. | en |
dc.contributor.committeemember | Moses, Hal L. | en |
dc.contributor.committeemember | Patterson, G. T. | en |
dc.contributor.department | Mechanical Engineering | en |
dc.date.accessioned | 2014-08-13T14:38:59Z | en |
dc.date.available | 2014-08-13T14:38:59Z | en |
dc.date.issued | 1986 | en |
dc.description.abstract | A one-dimensional, stage-by-stage axial compression system mathematical model has been constructed which can describe system behavior during post-stall events such as surge and rotating stall. The model uses a numerical technique to solve the nonlinear conservation equations of mass, momentum, and energy. Inputs for blade forces and shaft work are provided by a set of quasi-steady stage characteristics modified by a first order lagging equation to simulate dynamic stage characteristics. The model was validated with experimental results for a three-stage, low-speed compressor and a nine-stage, high-pressure compressor. Using these models, a parametric study was conducted to determine the effect of inlet resistance, combustor performance, heat transfer, and stage characteristic changes due to hardware modification on post—stall system behavior. | en |
dc.description.admin | incomplete_metadata | en |
dc.description.degree | Ph. D. | en |
dc.format.extent | xvi, 174 leaves | en |
dc.format.mimetype | application/pdf | en |
dc.identifier.uri | http://hdl.handle.net/10919/50002 | en |
dc.publisher | Virginia Polytechnic Institute and State University | en |
dc.relation.isformatof | OCLC# 16506477 | en |
dc.rights | In Copyright | en |
dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | en |
dc.subject.lcc | LD5655.V856 1986.D38 | en |
dc.subject.lcsh | Compressors | en |
dc.subject.lcsh | Gas-turbines | en |
dc.subject.lcsh | Stalling (Aerodynamics) | en |
dc.title | A stage-by-stage post-stall compression system modeling technique: methodology, validation, and application | en |
dc.type | Dissertation | en |
dc.type.dcmitype | Text | en |
thesis.degree.discipline | Mechanical Engineering | en |
thesis.degree.grantor | Virginia Polytechnic Institute and State University | en |
thesis.degree.level | doctoral | en |
thesis.degree.name | Ph. D. | en |
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