A BLADE ELEMENT THEORY BASED ACTUATOR DISK METHODOLOGY FOR MODELING OF FAN ENGINES IN RANS SIMULATIONS
AIAA Aviation Forum ; 2020 ; Online
Applied aerodynamics ; Volume 2 of 3 ; 1420-1438
2020
Conference paper
English
German Aerospace Center (DLR) | 2020
|Comparison and evaluation of blade element methods against RANS simulations and test data
Springer Verlag | 2022
|An Actuator Disk Model of Incidence and Deviation for RANS-Based Throughflow Analysis
Online Contents | 2014
|