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Effects of Nonuniform Blade Pitch on the Flow Through an Annular Turbine Nozzle

This paper discusses flow measurement results both upstream and downstream of a transonic annular gas turbine nozzle with a nonuniform pitch. The downstream measurements are performed in the plane where the leading edge of the rotor blade is located in the gas turbine. The experiments were performed...

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Detalhes bibliográficos
Autor principal: Rainer Kurz
Formato: Artigo
Idioma:Inglês
Publicado em: Hindawi Limited 1995-01-01
Colecção:International Journal of Rotating Machinery
Assuntos:
Acesso em linha:http://dx.doi.org/10.1155/S1023621X95000212
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