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Projektleitung:
Prof. Markus Klein
Institut:
LRT 1 - Institut für Angewandte Mathematik und Wissenschaftliches Rechnen 
Fakultät:
Fakultät für Luft- und Raumfahrttechnik 
Projektbezeichnung:
Analysis of Unsteady Effects in Fighter Aircraft Aerodynamics 
Projektbeschreibung:
The overall goal of the project is to obtain a better understanding of complex unsteady effects which are important for fighter aircraft aerodynamics. The simulation data includes systematic studies of the most important parameters and will be benchmarked with available data from literature as well as data from Airbus. After validation a detailed analysis of the data will help gaining a better understanding of the physics involved. Furthermore, the possibility of deriving simplified engineering...    »
 
Drittmittelgeber:
Airbus Defence and Space GmbH 
Datum Projektbeginn:
01.03.2020 
Datum Projektende:
31.03.2024