標(biāo)題: Titlebook: Advanced Aircraft Understanding via the Virtual Aircraft Model; Results of the Germa Ralf Heinrich Book 2025 Deutsches Zentrum für Luft- un [打印本頁] 作者: Iodine 時間: 2025-3-21 18:38
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書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model影響因子(影響力)學(xué)科排名
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書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model被引頻次
書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model被引頻次學(xué)科排名
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書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model年度引用學(xué)科排名
書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model讀者反饋
書目名稱Advanced Aircraft Understanding via the Virtual Aircraft Model讀者反饋學(xué)科排名
作者: ENNUI 時間: 2025-3-21 21:58
High-Fidelity Simulation for?Identification of?Steady and?Dynamic Transport Aircraft DerivativesA parameter identification process uses?time histories of a multidisciplinary flight dynamics simulation including rigid body and elastic degrees?of freedom together with the time dependent control surface inputs to estimate steady and dynamic derivatives. The focus is on the identification of the l作者: 澄清 時間: 2025-3-22 01:25 作者: 免費 時間: 2025-3-22 07:37 作者: 敵意 時間: 2025-3-22 10:45 作者: 吞沒 時間: 2025-3-22 16:29 作者: SCORE 時間: 2025-3-22 20:12
Overview and?Results of?Subproject VitAMIn-ABCcreasing the efficiency of computing large datasets, increasing the accuracy of the turbulence modelling by employing a local approach, the increased automation of the codes to reduce the human effort involved in the data generation, as well as additional activities improving the simulation capabili作者: 四海為家的人 時間: 2025-3-22 21:31
Spalart-Allmaras Turbulence Model Conditioning for Leading-Edge Vortex Flowsntains a significant grade of complexity and interest in the research community. This plays a major factor for the discrepancies with experimental or high fidelity data. A baseline common turbulence model is enhanced by means of a series of additional destruction terms which are formulated with a co作者: 獸皮 時間: 2025-3-23 04:17 作者: 夾克怕包裹 時間: 2025-3-23 08:02
VitAM-Flex—Computational Modelling and?Simulation to?Study Effects of?Elastic Aircraft Structures on. To reduce computational efforts, methods to establish a structural reduced-order model and its applicability for flexible aircraft configurations are studied. To gain a better understanding of the underlying flight physics, higher-order aeroelastic modelling approaches are used through coupled CFD作者: encomiast 時間: 2025-3-23 12:36 作者: Spangle 時間: 2025-3-23 16:05 作者: Nerve-Block 時間: 2025-3-23 20:48
Grundlagen der Berechnungsverfahrene studied. To gain a better understanding of the underlying flight physics, higher-order aeroelastic modelling approaches are used through coupled CFD-CSM techniques. Lastly, the impact of nonlinearities owing to large deformations on the prediction accuracy when using state-of-the-art flutter prediction methods is analysed.作者: BLANC 時間: 2025-3-24 02:01
Overview and?Results of?Subproject VitAMIn-ABCautomation of the codes to reduce the human effort involved in the data generation, as well as additional activities improving the simulation capabilities of the software. Most of the goals of the project were reached or surpassed, resulting in a considerable impact on the tools and processes in use at Airbus D&S.作者: Occupation 時間: 2025-3-24 03:37
VitAM-Flex—Computational Modelling and?Simulation to?Study Effects of?Elastic Aircraft Structures one studied. To gain a better understanding of the underlying flight physics, higher-order aeroelastic modelling approaches are used through coupled CFD-CSM techniques. Lastly, the impact of nonlinearities owing to large deformations on the prediction accuracy when using state-of-the-art flutter prediction methods is analysed.作者: 基因組 時間: 2025-3-24 07:01
Book 2025rcraft industry. The project was funded by the Ministry for Economic Affairs and Climate Action. In the book, different subprojects are presented, with their corresponding case studies. Readers will find extensive information on simulation strategies required for virtual flight testing, and verifica作者: harpsichord 時間: 2025-3-24 13:10 作者: Optimum 時間: 2025-3-24 17:08
Robustness Improvements for a Differential Reynolds Stress Modeling Using a Logarithmic Formulation carried out by comparing the predictions with SSG/LRR-. predictions and experimental data for complex industry relevant configurations. Comparison studies show that the new version of the model improves the robustness and convergence of computations while delivering predictions similar to the SSG/LRR-. predictions.作者: Awning 時間: 2025-3-24 21:09 作者: 集聚成團(tuán) 時間: 2025-3-25 01:32
Bayesian Calibration of?Extended Menter-SST Turbulence Model for?Vortical Flowss. A data driven calibration approach is employed based on Bayesian modeling to determine the coefficients of the extended turbulence model. Performance of the extended model is studied with complex delta wings under subsonic flow conditions.作者: 減去 時間: 2025-3-25 05:57 作者: 極深 時間: 2025-3-25 08:27
Tragwerksmodelle der Stabstatikimental data. The numerical accuracy is augmented for a certain cluster of cases around the calibration case in the parametric space which describes the classification of vortex flows over highly swept aerodynamic planforms.作者: 很是迷惑 時間: 2025-3-25 12:46 作者: 間諜活動 時間: 2025-3-25 16:08
Spalart-Allmaras Turbulence Model Conditioning for Leading-Edge Vortex Flowsimental data. The numerical accuracy is augmented for a certain cluster of cases around the calibration case in the parametric space which describes the classification of vortex flows over highly swept aerodynamic planforms.作者: cluster 時間: 2025-3-25 20:25
https://doi.org/10.1007/978-3-8348-9862-3 carried out by comparing the predictions with SSG/LRR-. predictions and experimental data for complex industry relevant configurations. Comparison studies show that the new version of the model improves the robustness and convergence of computations while delivering predictions similar to the SSG/LRR-. predictions.作者: Spinal-Fusion 時間: 2025-3-26 02:48
Eigenschaften statisch unbestimmter Systemeis adopted for the system identification process. The time domain system identification for the flexible aircraft was split in two parts: first the rigid-body dynamics were identified and then a new process to estimate the structural dynamics was developed and applied. Results for both parts will be shown.作者: Paleontology 時間: 2025-3-26 08:14
Zustandslinien statisch bestimmter Systemes. A data driven calibration approach is employed based on Bayesian modeling to determine the coefficients of the extended turbulence model. Performance of the extended model is studied with complex delta wings under subsonic flow conditions.作者: crutch 時間: 2025-3-26 09:09 作者: 沒血色 時間: 2025-3-26 15:38
https://doi.org/10.1007/978-3-8348-9862-3hods for the high fidelity, CFD-based aerodynamics,?the flight mechanics, and the structural dynamics. The test case is a narrow-body jet airliner for which?the simulation models and the results of two flight dynamics simulations for system identification as well as?a gust load alleviation scenario 作者: Meditative 時間: 2025-3-26 17:25
Tragwerksmodelle der Stabstatikospheric turbulence. It can be shown, that the aerodynamic response of the aircraft, relevant in terms of flight dynamics and passenger comfort, is well represented by the wing without considering the loads occurring on flap track fairings or engine. Since especially the engine has relevant contribu作者: 聽覺 時間: 2025-3-27 00:50
Overview of?Sub-Project y is the ability to enable . based on high-fidelity simulation tools. The progress made within the national research project . (.) by the German Aerospace Center (DLR) in the recent past regarding the development, validation and demonstration of methods and tools to perform virtual flight tests is p作者: esoteric 時間: 2025-3-27 01:21
High-Fidelity Simulation for?Identification of?Steady and?Dynamic Transport Aircraft Derivativeshods for the high fidelity, CFD-based aerodynamics,?the flight mechanics, and the structural dynamics. The test case is a narrow-body jet airliner for which?the simulation models and the results of two flight dynamics simulations for system identification as well as?a gust load alleviation scenario 作者: Countermand 時間: 2025-3-27 08:56 作者: frozen-shoulder 時間: 2025-3-27 09:36
1612-2909 eneration of aerodynamic databases. It addresses both researchers and professionals in the field of aviation engineering..978-3-031-69427-1978-3-031-69425-7Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: essential-fats 時間: 2025-3-27 16:28
Advanced Aircraft Understanding via the Virtual Aircraft ModelResults of the Germa作者: Supplement 時間: 2025-3-27 21:31
Advanced Aircraft Understanding via the Virtual Aircraft Model978-3-031-69425-7Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: Nausea 時間: 2025-3-28 01:40 作者: Ligneous 時間: 2025-3-28 03:59
Notes on Numerical Fluid Mechanics and Multidisciplinary Designhttp://image.papertrans.cn/b/image/167138.jpg作者: 解凍 時間: 2025-3-28 08:33 作者: 深淵 時間: 2025-3-28 10:43 作者: 大喘氣 時間: 2025-3-28 16:15
https://doi.org/10.1007/978-3-8348-9862-3riable is developed within the Vitam project and implemented into the DLR-TAU code. A verification and validation of the model implementation are conducted using several test cases which covered wall bounded flows as well as separating flows. Performance assessment of the new version of the model is作者: 悲觀 時間: 2025-3-28 22:05 作者: 個阿姨勾引你 時間: 2025-3-29 01:07
