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...
Main Authors: | Chana, K, Singh, UK, Povey, T |
---|---|
Format: | Journal article |
Sprog: | English |
Udgivet: |
2004
|
Lignende værker
-
EFFECT OF AGGRESSIVE INLET SWIRL ON HEAT TRANSFER AND AERODYNAMICS IN AN UNSHROUDED TRANSONIC HP TURBINE
af: Qureshi, I, et al.
Udgivet: (2012) -
Effect of a combined hot-streak and swirl profile on cooled 1.5-stage turbine aerodynamics: an experimental and computational study
af: Adams, MG, et al.
Udgivet: (2021) -
Improved methodologies for time-resolved heat transfer measurements, demonstrated on an unshrouded transonic turbine casing
af: Collins, M, et al.
Udgivet: (2016) -
Heat transfer and aerodynamics of an intermediate pressure nozzle guide vane with and without inlet temperature non-uniformity
af: Chana, K, et al.
Udgivet: (2003) -
Effect of low-NO X combustor swirl clocking on intermediate turbine duct vane aerodynamics with an upstream high pressure turbine stage — An experimental and computational study
af: Johansson, M, et al.
Udgivet: (2016)