Impact of trailing edge overhang length on the loss characteristics of fully cooled transonic nozzle guide vanes
The trailing edge (TE) design of a cooled high-pressure (HP) nozzle guide vane (NGV) requires consideration of both cooling and aerodynamic performances. Two designs are in common use: the centered-ejection design, in which coolant is ejected through a slot in the TE with roughly symmetrical suction...
Главные авторы: | Burdett, D, Povey, T |
---|---|
Формат: | Journal article |
Язык: | English |
Опубликовано: |
ASME International
2022
|
Схожие документы
-
Experimental and numerical analysis of loss characteristics of cooled transonic nozzle guide vanes
по: Povey, T, и др.
Опубликовано: (2022) -
Understanding capacity sensitivity of cooled transonic nozzle guide vanes: a parametric experimental and computational study of the impact of trailing edge geometry
по: Burdett, D, и др.
Опубликовано: (2021) -
Sensitivity of high pressure nozzle guide vane capacity to trailing edge cooling
по: Burdett, D
Опубликовано: (2021) -
An investigation of the effects of nozzle guide vane trailing edge cooling on rotor heat transfer in a transonic turbine stage
по: Gleixner, Aaron J. (Aaron James)
Опубликовано: (2008) -
Dendritic cooling for nozzle guide vanes
по: Batstone, JJR
Опубликовано: (2011)