A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes
55th AIAA Aerospace Sciences Meeting
2017-01-01
Conference paper
Electronic Resource
English
A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes (AIAA 2017-0109)
British Library Conference Proceedings | 2017
|Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes
Online Contents | 2009
|Computational Study of Combustor–Turbine Interactions
AIAA | 2018
|Computational Study of Combustor-Turbine Interactions
AIAA | 2017
|