dc.contributor.advisor | Rao, Balusu M. | |
dc.creator | White, Gary P. | |
dc.date.accessioned | 2022-04-04T13:50:33Z | |
dc.date.available | 2022-04-04T13:50:33Z | |
dc.date.issued | 1976 | |
dc.identifier.uri | https://hdl.handle.net/1969.1/CAPSTONE-RandT_1990 | |
dc.description | Program year: 1975/1976 | en |
dc.description | Digitized from print original stored in HDR | en |
dc.description.abstract | A 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.extent | 51 pages | en |
dc.format.medium | electronic | en |
dc.format.mimetype | application/pdf | |
dc.subject | flutter analysis | en |
dc.subject | airfoil | en |
dc.subject | infinite blades | en |
dc.subject | airloads | en |
dc.subject | cascade parameters | en |
dc.subject | flow parameters | en |
dc.subject | inter-blade spacing | en |
dc.subject | stagger angle | en |
dc.subject | phase angle | en |
dc.subject | Mach number | en |
dc.subject | frequency | en |
dc.title | Flutter Analysis Of A Cascade Of Rotor Blades | en |
dc.title.alternative | FLUTTER ANALYSIS OF A CASCADE OF ROTOR BLADES | en |
dc.type | Thesis | en |
thesis.degree.department | Aerospace Engineering | en |
thesis.degree.grantor | University Undergraduate Fellow | en |
thesis.degree.level | Undergraduate | en |
dc.type.material | text | en |