標(biāo)題: Titlebook: AeroStruct: Enable and Learn How to Integrate Flexibility in Design; Contributions to the Ralf Heinrich Conference proceedings 2018 Springe [打印本頁] 作者: 漏出 時間: 2025-3-21 16:23
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design影響因子(影響力)
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design影響因子(影響力)學(xué)科排名
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design網(wǎng)絡(luò)公開度
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design被引頻次
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design被引頻次學(xué)科排名
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design年度引用
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design年度引用學(xué)科排名
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design讀者反饋
書目名稱AeroStruct: Enable and Learn How to Integrate Flexibility in Design讀者反饋學(xué)科排名
作者: epicardium 時間: 2025-3-21 21:28 作者: 開花期女 時間: 2025-3-22 00:43 作者: 欲望 時間: 2025-3-22 07:57
Zusammenfassung der Arbeitsergebnisseatic divergence has to be avoided by using anisotropic properties of stiffened panels made of CFRP (carbon fibre reinforced plastic). The structural design includes parametric model generation and automated sizing of composite wings. An analytical formulation of stiffened panels is used to investiga作者: optic-nerve 時間: 2025-3-22 09:59
Bilanz der Verwaltungsreform in Deutschlandsign and optimization process. The optimization procedure is based on the Three-Columns-Concept, using a state-of the-art Finite-Element-Method (FEM) software for structural analysis purposes embedded into a multidisciplinary optimization software. The optimization model is formulated for traditiona作者: Grievance 時間: 2025-3-22 15:56
Personal und Personalcontrollingol modules for considering the influence of flight control functions in preliminary aircraft design. In order to improve the methods used for the design process, an automated tool chain was set up, that builts a flight-mechanical model of the airplane, calculates controller parameters according to c作者: outrage 時間: 2025-3-22 20:15 作者: dissolution 時間: 2025-3-22 22:00 作者: 愛社交 時間: 2025-3-23 02:32 作者: pacifist 時間: 2025-3-23 08:57 作者: JECT 時間: 2025-3-23 10:32
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作者: Optometrist 時間: 2025-3-23 13:58
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作者: 不愿 時間: 2025-3-23 19:41 作者: Corporeal 時間: 2025-3-24 01:16 作者: 愚笨 時間: 2025-3-24 05:10
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作者: Conquest 時間: 2025-3-24 06:37 作者: 的事物 時間: 2025-3-24 13:28
AeroStruct: Enable and Learn How to Integrate Flexibility in Design978-3-319-72020-3Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: Defense 時間: 2025-3-24 15:32 作者: 獨白 時間: 2025-3-24 20:04
978-3-319-89131-6Springer International Publishing AG 2018作者: GULP 時間: 2025-3-25 01:04
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作者: 容易生皺紋 時間: 2025-3-25 05:10 作者: 使絕緣 時間: 2025-3-25 08:34 作者: 我的巨大 時間: 2025-3-25 11:43
Development of Flight Control Functions for?Integration in Gust Load Simulationsol modules for considering the influence of flight control functions in preliminary aircraft design. In order to improve the methods used for the design process, an automated tool chain was set up, that builts a flight-mechanical model of the airplane, calculates controller parameters according to c作者: Ascribe 時間: 2025-3-25 16:58
Introduction to Airbus Use-Case “FlexCraft”An important aspect was to improve the collaboration between the disciplines like Aerodynamics, Loads or Structure. There was a lot of learning on requirements on fidelity and accuracy, but also about effects of uncertainties on the design. Multiple layer models of different fidelity helped to under作者: vasospasm 時間: 2025-3-25 23:55
On Recent Advances in Industrial High-Fidelity Aeroelasticityr nowadays aerodynamic prediction, the level of detail in the structural model is often limited to linear FEM models with, by definition, rigid airfoils. Here the usage of multi-body models with nonlinear body motion and single-body nonlinear structural models is presented. For dynamic applications 作者: white-matter 時間: 2025-3-26 03:04 作者: 提名 時間: 2025-3-26 06:18 作者: depreciate 時間: 2025-3-26 10:18
Treating Non-conforming Sensitivity Fields by Mortar Mapping and Vertex Morphing for Multi-disciplindemonstrate 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作者: 哀求 時間: 2025-3-26 16:08
Interfacing MSC Nastran to the CFD-Solver DLR-Tau for Unsteady FSI Analyses with Nonlinear Aircraft ose 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作者: LAPSE 時間: 2025-3-26 18:45 作者: 輕彈 時間: 2025-3-27 00:38 作者: 懸崖 時間: 2025-3-27 04:41
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作者: 相信 時間: 2025-3-27 06:45 作者: tariff 時間: 2025-3-27 11:59 作者: venous-leak 時間: 2025-3-27 15:13
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.作者: 調(diào)情 時間: 2025-3-27 21:39
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.作者: Minutes 時間: 2025-3-27 23:07
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.作者: molest 時間: 2025-3-28 04:18
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.作者: 尊嚴(yán) 時間: 2025-3-28 06:48
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.作者: 思考 時間: 2025-3-28 12:21
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.作者: 提名 時間: 2025-3-28 18:07 作者: 繁忙 時間: 2025-3-28 21:37
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.作者: 心胸狹窄 時間: 2025-3-28 23:23
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.作者: Palpable 時間: 2025-3-29 04:12 作者: 使乳化 時間: 2025-3-29 11:11 作者: geriatrician 時間: 2025-3-29 15:03 作者: Jubilation 時間: 2025-3-29 18:03 作者: 泥瓦匠 時間: 2025-3-29 20:53 作者: Blemish 時間: 2025-3-30 00:49
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.作者: Lyme-disease 時間: 2025-3-30 06:55 作者: cardiac-arrest 時間: 2025-3-30 09:14
https://doi.org/10.1007/978-3-322-81674-0f composite material. Thus, this paper aims at mathematical methods for topology optimization of the wing interior made of isotropic material, the optimization of orthotropic composite material in the wing hull and the proper treatment of practical deformation aspects and multiple loads in this context.
