In this paper we present activities of work package 3 (WP3), “Virtual Flight Test”, of the German Aerospace Center (DLR) Project VicToria. The mission of WP3 is the multidisciplinary numerical simulation of jet transport aircraft including flight mechanics, aerodynamics, and structural Dynamics. Aerodynamic modeling focuses on a CFD method solving the URANS equations using the DLR TAU code together with a HPC framework to enable massively parallel simulations. Similar research activities in the past have shown promising results, where the superiority of the CFD-based approach compared to Low-Fidelity methods was demonstrated
In this paper some of the current results of the "Aerodynamic Simulation of Unsteady Manoeuvres...
For some time computational fluid dynamics (CFD) based numerical simulations are an essential compon...
AbstractSome years ago the national CFD project MEGAFLOW was initiated in Germany to combine many of...
A multidisciplinary simulation environment based on the DLR TAU code has been developed which allows...
The virtual determination of aerodynamic loads of a transport aircraft taking into account aero-elas...
Numerical simulation is already an important cornerstone for aircraft design, although the applicati...
A crucial issue in the development process of a modern jet transport aircraft is the comprehensive e...
Within the DLR-Project SikMa-„Simulation komplexer Manöver“ („Simulation of Complex Maneuvers“) the ...
The procedure of realizing aerodynamic aspects of experimental and numerical manoeuvre simulations o...
This report presents first results in the application of the DLR TAU-code to the topic of engine/air...
To enable a realistic assessment of the aeroelastic phenomena of aircraft, a simultaneous applicatio...
Abstract: The procedure of realizing aerodynamic aspects of experimental and numerical manoeuvre sim...
The estimation of aerodynamic loads of a transport aircraft taking into account static aero-elastic ...
A crucial part of the design and certification process of a transport aircraft is the identification...
This report presents a novel CFD–flight mechanics approach and its evaluation. It is part of the wor...
In this paper some of the current results of the "Aerodynamic Simulation of Unsteady Manoeuvres...
For some time computational fluid dynamics (CFD) based numerical simulations are an essential compon...
AbstractSome years ago the national CFD project MEGAFLOW was initiated in Germany to combine many of...
A multidisciplinary simulation environment based on the DLR TAU code has been developed which allows...
The virtual determination of aerodynamic loads of a transport aircraft taking into account aero-elas...
Numerical simulation is already an important cornerstone for aircraft design, although the applicati...
A crucial issue in the development process of a modern jet transport aircraft is the comprehensive e...
Within the DLR-Project SikMa-„Simulation komplexer Manöver“ („Simulation of Complex Maneuvers“) the ...
The procedure of realizing aerodynamic aspects of experimental and numerical manoeuvre simulations o...
This report presents first results in the application of the DLR TAU-code to the topic of engine/air...
To enable a realistic assessment of the aeroelastic phenomena of aircraft, a simultaneous applicatio...
Abstract: The procedure of realizing aerodynamic aspects of experimental and numerical manoeuvre sim...
The estimation of aerodynamic loads of a transport aircraft taking into account static aero-elastic ...
A crucial part of the design and certification process of a transport aircraft is the identification...
This report presents a novel CFD–flight mechanics approach and its evaluation. It is part of the wor...
In this paper some of the current results of the "Aerodynamic Simulation of Unsteady Manoeuvres...
For some time computational fluid dynamics (CFD) based numerical simulations are an essential compon...
AbstractSome years ago the national CFD project MEGAFLOW was initiated in Germany to combine many of...