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dc.contributor.advisorRao, Balusu M.
dc.creatorWhite, Gary P.
dc.date.accessioned2022-04-04T13:50:33Z
dc.date.available2022-04-04T13:50:33Z
dc.date.issued1976
dc.identifier.urihttps://hdl.handle.net/1969.1/CAPSTONE-RandT_1990
dc.descriptionProgram year: 1975/1976en
dc.descriptionDigitized from print original stored in HDRen
dc.description.abstractA classical two-dimensional, bending-torsion flutter analysis of a reference airfoil in a cascade of infinite blades is performed. The unsteady airloads on the reference airfoil are predicted using a numerical lifting surface theory. Several cascade and flow parameters such as inter-blade spacing, stagger angle, phase angle between blades, Mach number, and frequency are investigated. The bending-torsion flutter speed of the cascaded reference airfoil is studied as a function of the cascade and flow parameters and the results are compared with that of an isolated airfoil.en
dc.format.extent51 pagesen
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.subjectflutter analysisen
dc.subjectairfoilen
dc.subjectinfinite bladesen
dc.subjectairloadsen
dc.subjectcascade parametersen
dc.subjectflow parametersen
dc.subjectinter-blade spacingen
dc.subjectstagger angleen
dc.subjectphase angleen
dc.subjectMach numberen
dc.subjectfrequencyen
dc.titleFlutter Analysis Of A Cascade Of Rotor Bladesen
dc.title.alternativeFLUTTER ANALYSIS OF A CASCADE OF ROTOR BLADESen
dc.typeThesisen
thesis.degree.departmentAerospace Engineeringen
thesis.degree.grantorUniversity Undergraduate Fellowen
thesis.degree.levelUndergraduateen
dc.type.materialtexten


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