Boundary layer calculation of an effusion cooled turbine blade
16th Aerospace Sciences Meeting ; 1978 ; Huntsville , AL , U.S.A.
1978-01-01
Conference paper
Electronic Resource
English
Some experiments on an effusion cooled turbine nozzle blade
TIBKAT | 1956
|A theoretical note on effusion cooled gas turbine blades
TIBKAT | 1954
|Manufacturing of Effusion Cooled Combustors
SAE Technical Papers | 1991
|Effusion Cooled CMC Rocket Combustion Chamber
AIAA | 2005
|Three-Dimensional Boundary Layer in a Turbine Blade Passage
Online Contents | 2017
|