Effect of Hot Streak on Aerothermal Performance of High Pressure Turbine Guide Vane under Different Swirl Intensities

In advanced civil aero-engine, the gas exiting combustor typically features hot streak (HS) and swirl that affect the aerothermal performances of the high pressure (HP) nozzle guide vane (NGV). The purpose of this paper is to study the influences of HS on HP NGV aerothermal behaviors under swirl wit...

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Bibliographic Details
Main Authors: Shenghui Zhang, Shuiting Ding, Peng Liu, Tian Qiu
Format: Article
Language:English
Published: MDPI AG 2022-10-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/9/10/579

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