The finite element method applied to flows in turbomachines.
dc.contributor.advisor | Collins, Daniel J. | |
dc.contributor.author | Gavito, Valentin Francisco Jr. | |
dc.date | December 1976 | |
dc.date.accessioned | 2012-11-16T18:47:40Z | |
dc.date.available | 2012-11-16T18:47:40Z | |
dc.date.issued | 1976-12 | |
dc.identifier.uri | http://hdl.handle.net/10945/17777 | |
dc.description.abstract | The finite element method is applied to The two-dimensional, inviscid, compressible radial equilibrium equation for axial compressors. Isoparametric elements are used along with three-point Gaussian integration for stiffness matrix evaluation. The radial equilibrium equation is put into quasi-harmonic form for stream function formulation and results are presented using an isentropic flow assumption. Axial velocity profiles at rotor and stator blade edges are compared with published performance data of the NASA Task-1 stage transonic compressor and with numerical finite element results of Hirsch and Warzee. | |
dc.description.uri | http://archive.org/details/thefiniteelement1094517777 | |
dc.language.iso | en_US | |
dc.rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. | |
dc.subject.lcsh | Aeronautics | en_US |
dc.title | The finite element method applied to flows in turbomachines. | en_US |
dc.type | Thesis | en_US |
dc.contributor.secondreader | Shreeve, Raymond P. | |
dc.contributor.corporate | Naval Postgraduate School (U.S.) | |
dc.contributor.department | Aeronautics | |
dc.subject.author | finite element method | en_US |
dc.subject.author | turbomachines | en_US |
dc.description.service | Lieutenant, United States Navy | |
etd.thesisdegree.name | M.S. in Aeronautical Engineering | en_US |
etd.thesisdegree.level | Masters | en_US |
etd.thesisdegree.discipline | Aeronautical Engineering | en_US |
etd.thesisdegree.grantor | Naval Postgraduate School | en_US |
dc.description.distributionstatement | Approved for public release; distribution is unlimited. |
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