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Contenido archivado el 2024-04-30

The asymptotic theory of noise generation by rotating blade rows

Objetivo



At the University of Cambridge, Applied Mathematics, and under the supervision of Dr. N. Peake, I hope to study the interaction of vorticity with a rotating blade row of an aeroengine, enabling the prediction and understanding of the generation of sound of such engines. This three-year Ph.D. study could make a significant contribution to Europe's efforts to contain the aircraft noise pollution around its airports.
Peake has developed solutions for the case that the blade row consists of flat, zerothickness blades. The proposed research aims at determining the effects of camber and thickness of the blades on the sound generation. The principle mathematical tool will be asymptotic analysis, although other analytical and numerical methods will also be applied to the fields of acoustics and unsteady aerodynamics.

Ámbito científico (EuroSciVoc)

Programa(s)

Tema(s)

Convocatoria de propuestas

Datos no disponibles

Régimen de financiación

RGI - Research grants (individual fellowships)

Coordinador

University of Cambridge
Aportación de la UE
Sin datos
Dirección
Silver Street
CB3 9EW Cambridge
Reino Unido
Coste total
Sin datos

Participantes (1)