HP Vane Aerodynamics and Heat Transfer in the Presence of Aggressive Inlet Swirl
Modern lean burn combustors now employ aggressive swirlers to enhance fuel-air mixing and improve flame stability. The flow at combustor exit can therefore have high residual swirl. A good deal of research concerning the flow within the combustor is available in open literature. The impact of swirl...
Egile Nagusiak: | Qureshi, I, Smith, A, Povey, T |
---|---|
Formatua: | Journal article |
Hizkuntza: | English |
Argitaratua: |
2013
|
Antzeko izenburuak
-
HP VANE AERODYNAMICS AND HEAT TRANSFER IN THE PRESENCE OF AGGRESSIVE INLET SWIRL
nork: Qureshi, I, et al.
Argitaratua: (2012) -
EFFECT OF AGGRESSIVE INLET SWIRL ON HEAT TRANSFER AND AERODYNAMICS IN AN UNSHROUDED TRANSONIC HP TURBINE
nork: Qureshi, I, et al.
Argitaratua: (2012) -
Effect of Aggressive Inlet Swirl on Heat Transfer and Aerodynamics in an Unshrouded Transonic HP Turbine
nork: Qureshi, I, et al.
Argitaratua: (2012) -
Heat transfer and aerodynamics of an intermediate pressure nozzle guide vane with and without inlet temperature non-uniformity
nork: Chana, K, et al.
Argitaratua: (2003) -
EFFECT OF STIMULATED COMBUSTOR TEMPERATURE NONUNIFORMITY ON HP VANE AND ENDWALL HEAT TRANSFER: AN EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION
nork: Qureshi, I, et al.
Argitaratua: (2010)