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...

Täydet tiedot

Bibliografiset tiedot
Päätekijät: Chana, K, Singh, UK, Povey, T
Aineistotyyppi: Journal article
Kieli:English
Julkaistu: 2004