Proclaim 发表于 2025-3-25 05:59:22

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皮萨 发表于 2025-3-25 08:21:16

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defile 发表于 2025-3-25 14:35:56

Entwicklung Stimmdiagnostischer Methoden,have been investigated. As central test cases a generic wing-aileron configuration based on the LANN wing was studied. Approaches based on mesh deformation, the Chimera technique and a combination of Chimera technique and mesh deformation were considered. As second test case a generic wing-spoil

使残废 发表于 2025-3-25 16:46:39

Entwicklung Stimmdiagnostischer Methoden,he development and the assessment of a simplified approach that uses existing and well verified scattered data interpolation methods. The interpolation problem is addressed by a pragmatic partitioning approach of large models. Analysis of the interpolation of deflections between different discretiza

禁止 发表于 2025-3-25 20:26:12

https://doi.org/10.1007/978-3-211-69361-2ta transfer between the aerodynamic surface and the structural model, and the CFD-mesh deformation are the key parameters. This paper shows a methodology to couple different CFD-solvers to the commercial finite element code Nastran. Thereby the coupling scheme can combine different coupling methods,

ENDOW 发表于 2025-3-26 00:08:20

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interpose 发表于 2025-3-26 07:29:54

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和蔼 发表于 2025-3-26 11:05:59

Entwicklung Stimmdiagnostischer Methoden,faces the dual meshes of the different blocks through cutting with an interface common for the blocks and is named the Dual Mesh Connect (DMC) approach. This approach is spatially conservative and capable of treating blocks with intersecting geometries in a natural manner. A description of the curre

Palpable 发表于 2025-3-26 13:08:39

Anatomie und Physiologie der Stimme,eraction between the periodically separating flow from the wing and the horizontal tail plane. Therefore a high resolved hexahedral block has been included into the wake area to propagate the turbulent structures. Two different approaches have been used to perform the simulations. First an unsteady

BIPED 发表于 2025-3-26 17:15:03

Nonlinear Reduced Order Modeling for Aeroelastic Simulation with Neural Networks,er modeling approaches are developed, for instance harmonic balance, center manifold, normal form and numerical continuation methods. An introduction to these methods can be found in Henshaw et al. . Other methods create a linear state-space formulation via the eigenvalue realization algorithm (ERA) used for example by Lucia et al. .
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查看完整版本: Titlebook: Computational Flight Testing; Results of the Closi Norbert Kroll,Rolf Radespiel,Kaare Sørensen Book 2013 Springer-Verlag Berlin Heidelberg