It is common practice in aircraft industry to perform maneuver and gust loads computations on the basis of potential theory aerodynamics methods that neglect important physical effects. In order to master the future challenges of aviation, however, there is a need for higher-precision loads computations. For this and other purposes, the RANS-CFD-based multidisciplinary simulation environment FlowSimulator is being developed. The status of selected features of the environment related to higher-precision maneuver simulations is presented; example applications are discussed
High-fidelity simulations play a key role for aircraft design, virtual flight testing and simulation...
Numerical simulation is already an important cornerstone for aircraft design, although the applicati...
The vision and final goal of DLR’s guiding concept of a virtual aircraft is the highly accurate nume...
The structural dimensioning of an aircraft is decisively influenced by gust, maneuver and ground loa...
The structural dimensioning of an airplane will be significantly influenced by gust, maneuver and gr...
In ComFliTe, a lot of work has been carried out to improve the multi-disciplinary simulation of free...
The application of CFD methods for the solution of the Euler and Reynolds-averaged Navier-Stokes equ...
Gust load analysis is a relevant part of the certification process of aircraft. In need of low compu...
A multidisciplinary simulation environment based on the DLR TAU code has been developed which allows...
Computational engineering methods play a more and more important role in building aircraft that move...
A software program and associated methodology to study gust loading on aircraft exists for a classif...
During aircraft design and certification, one of the most vital development tasks is the calculation...
This work presents results of dynamic 1-cos gust load simulations for a flying wing configuration. T...
A software program and associated methodology to study gust loading on aircraft exists for a classif...
The aim of this thesis is to set up a high-fidelity fluid structure interaction (FSI) simulation env...
High-fidelity simulations play a key role for aircraft design, virtual flight testing and simulation...
Numerical simulation is already an important cornerstone for aircraft design, although the applicati...
The vision and final goal of DLR’s guiding concept of a virtual aircraft is the highly accurate nume...
The structural dimensioning of an aircraft is decisively influenced by gust, maneuver and ground loa...
The structural dimensioning of an airplane will be significantly influenced by gust, maneuver and gr...
In ComFliTe, a lot of work has been carried out to improve the multi-disciplinary simulation of free...
The application of CFD methods for the solution of the Euler and Reynolds-averaged Navier-Stokes equ...
Gust load analysis is a relevant part of the certification process of aircraft. In need of low compu...
A multidisciplinary simulation environment based on the DLR TAU code has been developed which allows...
Computational engineering methods play a more and more important role in building aircraft that move...
A software program and associated methodology to study gust loading on aircraft exists for a classif...
During aircraft design and certification, one of the most vital development tasks is the calculation...
This work presents results of dynamic 1-cos gust load simulations for a flying wing configuration. T...
A software program and associated methodology to study gust loading on aircraft exists for a classif...
The aim of this thesis is to set up a high-fidelity fluid structure interaction (FSI) simulation env...
High-fidelity simulations play a key role for aircraft design, virtual flight testing and simulation...
Numerical simulation is already an important cornerstone for aircraft design, although the applicati...
The vision and final goal of DLR’s guiding concept of a virtual aircraft is the highly accurate nume...