Turbine heat transfer and aerodynamic measurements and predictions for A 1.5 Stage configuration

This paper considers the surface heat transfer rate to, and aerodynamics of, a 1.5 stage turbine - a high pressure (HP) turbine stage followed by an intermediate pressure (IP) vane. Unsteady interactions arising from the relative motions of vane/blade rows are examined. The IP vane was of structural...

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Detalhes bibliográficos
Principais autores: Chana, K, Singh, UK, Povey, T
Formato: Journal article
Idioma:English
Publicado em: 2004