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Titlebook: AeroStruct: Enable and Learn How to Integrate Flexibility in Design; Contributions to the Ralf Heinrich Conference proceedings 2018 Springe

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Further Development of CAA Simulation for Isolated and Installed Nozzle Configurationsly applied to isolated configurations of jet and airframe with different source models. For the prediction of jet noise, the source model as proposed by Tam and Auriault has been used for isolated nozzle configurations. A modeling approach for isolated airframe noise configurations is relying on the
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Personal und Personalcontrollinggn process, an automated tool chain was set up, that builts a flight-mechanical model of the airplane, calculates controller parameters according to consistent criteria and automatically implements flight control functions in a high fidelity simulation environment.
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Controlling deutscher TV-Sender dataformat as the core of the system. The system has been setup in a flexible and modular fashion such that components can be exchanged and the system can be applied to applications needing only a subset of the functionality. This article describes some of the integration details as well as applications with results.
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https://doi.org/10.1007/978-3-642-47911-3in the length-scale equation is implemented and calibrated, resulting in the JHh-v3 model. Simulations of practically relevant test cases with free shear layers are performed using the JHh-v2 and JHh-v3 turbulence models. For comparison, experimental data and results of simulations with the Menter-SST eddy-viscosity model are shown.
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Development of Flight Control Functions for Integration in Gust Load Simulationsgn process, an automated tool chain was set up, that builts a flight-mechanical model of the airplane, calculates controller parameters according to consistent criteria and automatically implements flight control functions in a high fidelity simulation environment.
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Application of Adjoint Based Optimization on a MALE Platform dataformat as the core of the system. The system has been setup in a flexible and modular fashion such that components can be exchanged and the system can be applied to applications needing only a subset of the functionality. This article describes some of the integration details as well as applications with results.
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Application of Reynolds-Stress-Models on Free Shear Layersin the length-scale equation is implemented and calibrated, resulting in the JHh-v3 model. Simulations of practically relevant test cases with free shear layers are performed using the JHh-v2 and JHh-v3 turbulence models. For comparison, experimental data and results of simulations with the Menter-SST eddy-viscosity model are shown.
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