Principal Investigator:
Daniela Gisele François
, Institut für Strömungsmechanik, TU Braunschweig (Germany)
HPC Platform used:
Hermit of HLRS
Local Project ID:
NSESRSM
One of the major limiting factors of the flight operational range of transport aircraft is the inlet separation of engine. The overall aim of this project is to provide an efficient numerical method able to compute the large range of spectral scales present in flows during the separation process.