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

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Numerical Computations of Isolated and Installed Engine Jet Flowsuse of the DLR TAU-Code to investigate the complex aerodynamics of jet-flap interactions was devised which also ensures the usability of the RANS (Reynolds Averaged Navier–Stokes) results in a subsequent aeroacoustic analysis.

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Further Development of CAA Simulation for Isolated and Installed Nozzle Configurationsnsideration of both noise generation mechanisms simultaneously. Thus, a vorticity based ‘Eddy Relaxation’ source model has been recently proposed as further development of this methodology, which is expected to capture the installation effect.

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只看該作者 · 發(fā)表于 2025-3-30 00:49:14

Ausgangssituation im Anlagenbau,use of the DLR TAU-Code to investigate the complex aerodynamics of jet-flap interactions was devised which also ensures the usability of the RANS (Reynolds Averaged Navier–Stokes) results in a subsequent aeroacoustic analysis.

只看該作者 · 發(fā)表于 2025-3-30 06:55:09

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