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...
المؤلفون الرئيسيون: | Burdett, D, Povey, T |
---|---|
التنسيق: | Journal article |
اللغة: | English |
منشور في: |
ASME International
2022
|
مواد مشابهة
-
Experimental and numerical analysis of loss characteristics of cooled transonic nozzle guide vanes
حسب: Povey, T, وآخرون
منشور في: (2022) -
Understanding capacity sensitivity of cooled transonic nozzle guide vanes: a parametric experimental and computational study of the impact of trailing edge geometry
حسب: Burdett, D, وآخرون
منشور في: (2021) -
Sensitivity of high pressure nozzle guide vane capacity to trailing edge cooling
حسب: Burdett, D
منشور في: (2021) -
An investigation of the effects of nozzle guide vane trailing edge cooling on rotor heat transfer in a transonic turbine stage
حسب: Gleixner, Aaron J. (Aaron James)
منشور في: (2008) -
Dendritic cooling for nozzle guide vanes
حسب: Batstone, JJR
منشور في: (2011)