JECT
发表于 2025-3-23 10:32:57
https://doi.org/10.1007/978-3-322-99239-0demonstrate the advantages of such a procedure in the context of shape optimization. It points out the importance of a common design control approach in a Multi-Disciplinary Optimization (MDO) environment. In particular, individual components of MDO have nonmatching interfaces when Fluid-Structure I
Optometrist
发表于 2025-3-23 13:58:37
https://doi.org/10.1007/978-3-658-42044-4ose the MSC Nastran solver provides a programming interface OpenFSI, which is used and extended here for a flexible usage. Target is the integration of this nonlinear structural solver into the parallel programming environment FlowSimulator in which the DLR-Tau code is used for fluid analysis. The d
不愿
发表于 2025-3-23 19:41:48
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Corporeal
发表于 2025-3-24 01:16:16
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愚笨
发表于 2025-3-24 05:10:23
Ausgangssituation im Anlagenbau,ly 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
Conquest
发表于 2025-3-24 06:37:06
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的事物
发表于 2025-3-24 13:28:57
AeroStruct: Enable and Learn How to Integrate Flexibility in Design978-3-319-72020-3Series ISSN 1612-2909 Series E-ISSN 1860-0824
Defense
发表于 2025-3-24 15:32:32
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独白
发表于 2025-3-24 20:04:09
978-3-319-89131-6Springer International Publishing AG 2018
GULP
发表于 2025-3-25 01:04:51
Integrated Process Chain for Aerostructural Wing Optimization and Application to an NLF Forward Swepure of this process chain enables two of the most promising future technologies in commercial aircraft design in the context of multidisciplinary design optimization (MDO). These technologies are natural laminar flow (NLF) and aeroelastic tailoring using carbon fiber reinforced plastics (CFRP). With