標題: Titlebook: Coupling of Fluids, Structures and Waves in Aeronautics; Proceedings of a Fre Noel G. Barton,Jacques Periaux Conference proceedings 2003 Sp [打印本頁] 作者: clot-buster 時間: 2025-3-21 16:30
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics影響因子(影響力)
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics影響因子(影響力)學科排名
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics網絡公開度
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics網絡公開度學科排名
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics被引頻次
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics被引頻次學科排名
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics年度引用
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics年度引用學科排名
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics讀者反饋
書目名稱Coupling of Fluids, Structures and Waves in Aeronautics讀者反饋學科排名
作者: motivate 時間: 2025-3-21 21:23 作者: pulse-pressure 時間: 2025-3-22 01:51
Dynamics and Control of Flames Interacting with Pressure Wavesion research. A number of related issues have been investigated over the last decades. Studies have concerned fundamental aspects and practical implications. Important progress has been accomplished in the understanding, modeling and simulation of combustion dynamics. Detailed experiments have provi作者: 放縱 時間: 2025-3-22 07:12 作者: Mucosa 時間: 2025-3-22 12:33
Application of Unsteady Fluid-Structure Methods to Problems in Aeronautics and Spaced the Center for Aerospace structure of University of Boulder. A particular focus is put on the fluid part, which involves the MUSCL-FEM technology relying on a vertex centered upwind finite volume formulation for unstructured tetrahedrizations, and a mesh deformation technique combined with an Arbi作者: 散步 時間: 2025-3-22 13:58
Numerical Simulation in Aeroelasticity For Complex Configurations in a Transonic Flowethod concerns the flutter simulation using the linearized Euler equations in the frequency domain. The second method concerns the direct fluid structure coupling in the time domain..The Euler/Navier-Stokes equations are solved on a multi-block structured mesh and are based on an ALE formulation. Sp作者: 散步 時間: 2025-3-22 20:43
Numerical Prediction of Flow Instabilities and Aeroelastic Effects of vortex breakdown, a fluid structure that bedevils high angle of attack aircraft but may assist the breakup of tip vortices, has been undertaken using an in-house parallelized spectral element code. Second, aeroelasticity has been identified as one of the most important problems presently facing 作者: 圓桶 時間: 2025-3-22 21:25 作者: FLIP 時間: 2025-3-23 03:21
Overview of Nonlinear Finite Element Modelling of Flexible Manoeuvring Aerospace Systems and Structueuvring systems and structures. The applications include robotics and aircraft wings. In the case of robotics, modeling of manipulators, which are capable of being reconfigured to perform various tasks, is carried out and results from simple models are compared with experimental data. In the case of作者: Flagging 時間: 2025-3-23 08:09 作者: Alpha-Cells 時間: 2025-3-23 09:50
High Performance Computation and Visualization of EMs Using an Integrated Computation Systemd discusses several different computational methods with emphasis on different problems requiring different computational methods. Several application problems of computational electromagnetics (CEMs) in the areas of electrical and electronic engineering and communications systems are presented. The作者: 長處 時間: 2025-3-23 16:14
Genetic Algorithm Optimisation of Mathematical Models — An Aircraft Structural Dynamics Case Studyial intelligence optimisation tool known as genetic algorithms (GAs) where the optimisation problem to be tackled involves creating a structural dynamic aircraft model that best matches the available experimental frequency response function (FRF) data. It will be demonstrated how the inverse structu作者: 上坡 時間: 2025-3-23 20:33
Evolutionary Algorithms for Multi-Objective Design Optimizationcal EAs are good enough for problems based on simple mathematical models (i.e. linear models) . However, as the applications evolve in complexity, we had to develop new algorithms with better capabilities: among these, we will mostly focus on algorithms combining EAs and Game Theory (hence enabling 作者: Pituitary-Gland 時間: 2025-3-23 22:59 作者: 殖民地 時間: 2025-3-24 05:41 作者: 色情 時間: 2025-3-24 09:22 作者: HOWL 時間: 2025-3-24 12:48 作者: ABASH 時間: 2025-3-24 14:55 作者: Assault 時間: 2025-3-24 19:08 作者: 拋物線 時間: 2025-3-24 23:25 作者: Throttle 時間: 2025-3-25 06:29 作者: 成份 時間: 2025-3-25 10:51 作者: 使虛弱 時間: 2025-3-25 12:57
Antenna Integration on Aircraft: Needs and MethodologyModern combat aircraft increasingly incorporate more and more operational functions. These functions use a wide range of frequencies over the entire electromagnetic spectrum. They are essentially related to three functional areas, which are:作者: 女上癮 時間: 2025-3-25 17:13
An Iterative Method for Time-harmonic Integral Maxwell’s EquationsWe present an iterative algorithm for time harmonic Maxwell’s equation, using a particular integral formulation proposed in [13], [8]. We discuss the rate of convergence of the algorithm. In the case of of sphere scatterer the condition number of the method is adressed by means of Fourier transform.作者: Obverse 時間: 2025-3-25 21:55
Techniques for Optimal Shape DesignIn this paper we apply to a few new problems some of the techniques we have developed over the years for optimal shape design. These include optimality conditions, automatic differentiation and the appropriate descent methods.作者: Fibrin 時間: 2025-3-26 01:48
An Investigation of the Least-Squares Finite Element Method in ElectromagnetismThe least-squares FEM applied directly to Maxwell’s equations is investigated as an alternative to the Galerkin FEM. The least-squares FEM is introduced via a simple model problem. Determinacy and ellipticity of the Maxwell system is investigated using Clifford algebra. Some simple results for a practical component are presented.作者: 不足的東西 時間: 2025-3-26 04:26
Das Wissen und die Wissensgesellschaft,edge segments are of approximately equal length and the region of separated flow at the junction of the wedges can extend over a significant fraction of the surface in uniform steady flow. The extent of the separation was found to be strongly dependent on the Mach and Knudsen numbers. A noise field 作者: 隱藏 時間: 2025-3-26 09:46 作者: 親屬 時間: 2025-3-26 12:39 作者: anagen 時間: 2025-3-26 20:32 作者: 擴音器 時間: 2025-3-26 22:16
Personbezogenes Wissensmanagement,d the Center for Aerospace structure of University of Boulder. A particular focus is put on the fluid part, which involves the MUSCL-FEM technology relying on a vertex centered upwind finite volume formulation for unstructured tetrahedrizations, and a mesh deformation technique combined with an Arbi作者: 不安 時間: 2025-3-27 02:06 作者: Neuralgia 時間: 2025-3-27 08:10
Das Wissen und die Wissensgesellschaft, of vortex breakdown, a fluid structure that bedevils high angle of attack aircraft but may assist the breakup of tip vortices, has been undertaken using an in-house parallelized spectral element code. Second, aeroelasticity has been identified as one of the most important problems presently facing 作者: 流浪者 時間: 2025-3-27 12:54
Fehlannahmen zum Wissensmanagement, modal actuator and modal sensor are designed by modulating the thickness of the piezoelectric actuator and sensor layers. In the second method, the distributed piezoelectric element (DPE) method, the modal actuator and sensor are designed based on segmentation of the piezoelectric actuator layer fu作者: llibretto 時間: 2025-3-27 17:24 作者: Proclaim 時間: 2025-3-27 17:55
Das Wissen und die Wissensgesellschaft,ion of Maxwell’s equations with prescribed boundary conditions. In general, the interpretation of radar returns involves the solution of inverse problems, which are essentially illposed, even in the linear case, so special procedures are necessary in order to obtain meaningful solutions..In this pap作者: 的’ 時間: 2025-3-27 23:07 作者: 陳舊 時間: 2025-3-28 03:54
Bildungsstandards und Verstehenskompetenzial intelligence optimisation tool known as genetic algorithms (GAs) where the optimisation problem to be tackled involves creating a structural dynamic aircraft model that best matches the available experimental frequency response function (FRF) data. It will be demonstrated how the inverse structu作者: 警告 時間: 2025-3-28 07:33 作者: Dignant 時間: 2025-3-28 12:58
Bildungsstandards und Verstehenskompetenzulting motion of the structure can then be quite important but is mainly composed of a large rigid body motion to which is superposed a small elastic perturbation. Due to its size, this perturbation can be modeled by the linearized elasticity equation. The resulting problem leads to nonlinear partia作者: 惰性女人 時間: 2025-3-28 16:31
Coupling of Fluids, Structures and Waves in Aeronautics978-3-540-44873-0Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: 沒有希望 時間: 2025-3-28 20:59
Dynamics and Control of Smart Structures Using Piezoelectric Actuators and Sensorslly covered on the host plate. In the third method, the quasi-modal sensors and quasi-modal actuators are developed using several piezoelectric patches, and optimization criteria are given for finding the optimal locations and sizes of these patches in order to minimize the observation and control spillovers.作者: 幸福愉悅感 時間: 2025-3-29 02:52 作者: mortgage 時間: 2025-3-29 03:05
Some Remarks on Fluid-Structure Interaction Problems in Case of Rigid Body plus Small Perturbationsl differential equations that can be coupled to the Navier—Stokes equations and numerically tackled by the use of modal expensions. The aim of this paper is to derive this formulation under clear assumptions.作者: 神刊 時間: 2025-3-29 10:24 作者: Gratulate 時間: 2025-3-29 13:37
Application of Unsteady Fluid-Structure Methods to Problems in Aeronautics and Spacelying on a vertex centered upwind finite volume formulation for unstructured tetrahedrizations, and a mesh deformation technique combined with an Arbitrary Lagrange-Euler formulation. Three typical applications will then be presented.作者: 心胸開闊 時間: 2025-3-29 16:29
Overview of Nonlinear Finite Element Modelling of Flexible Manoeuvring Aerospace Systems and Structuable of being reconfigured to perform various tasks, is carried out and results from simple models are compared with experimental data. In the case of aircraft, results from simulations involving an aerodynamically loaded aircraft wing model are presented.作者: cogitate 時間: 2025-3-29 20:36
Fehlannahmen zum Wissensmanagement,lly covered on the host plate. In the third method, the quasi-modal sensors and quasi-modal actuators are developed using several piezoelectric patches, and optimization criteria are given for finding the optimal locations and sizes of these patches in order to minimize the observation and control spillovers.作者: PATHY 時間: 2025-3-30 01:52
Bildungsstandards und Verstehenskompetenz paper also presents computational and visual electromagnetics (CVEM) using an integrated programming, integrated computation system and high performance parallel computer. The future trend of high performance computing and collaborative visualization for coupling problems is also described.作者: HIKE 時間: 2025-3-30 05:50
Bildungsstandards und Verstehenskompetenzl differential equations that can be coupled to the Navier—Stokes equations and numerically tackled by the use of modal expensions. The aim of this paper is to derive this formulation under clear assumptions.作者: Blood-Clot 時間: 2025-3-30 10:29 作者: FLIC 時間: 2025-3-30 16:01
Organisationsbezogenes Wissensmanagement,aspects of the phenomena involved. Accelerating reference frame solution techniques have recently been developed and employed in the study of bluff body aeroelasticity: these are described and applied to the study of flows past slender cylinders with prescribed motion, and with aeroelastic fluid-structure interaction.作者: A保存的 時間: 2025-3-30 16:33 作者: FEAT 時間: 2025-3-30 23:25 作者: 好忠告人 時間: 2025-3-31 04:16
Das Wissen und die Wissensgesellschaft,ttachment points were affected, but the extent of the separation did not change appreciably. Calculations were also made with an oscillation in the streamwise direction imposed on the body. The extent of the separation increased when the peak oscillation speed ceased to be small in comparison with the stream speed.作者: GNAT 時間: 2025-3-31 07:43
Das Wissen und die Wissensgesellschaft,ve spectrum from the Doppler spectrum of scattered radar signals, (ii) the determination of an unknown S-matrix observed through a polarisation-transforming medium, and (iii) the determination of the temporal signatures of a class of wave-wave interactions in the ionosphere.作者: CUMB 時間: 2025-3-31 12:29 作者: 幾何學家 時間: 2025-3-31 14:06 作者: 向宇宙 時間: 2025-3-31 18:48 作者: HEDGE 時間: 2025-3-31 23:10
Conference proceedings 2003nautics Industry", together with a summary of important themes and issues. This research promotes the advanced technologies necessary for continued development of efficient and environmentally sustainable transport systems..作者: extract 時間: 2025-4-1 02:46 作者: ordain 時間: 2025-4-1 08:07
Organisationsbezogenes Wissensmanagement,thout detracting from the accuracy and the robustness of the simulations. These numerical methods are applied for static aeroelasticity and flutter prediction for complex civil and military configurations in transonic flow. The tools are tested for a Limit Cycle Oscillations (LCO) problem in 2D.作者: Blasphemy 時間: 2025-4-1 11:04 作者: BROW 時間: 2025-4-1 15:42 作者: Focus-Words 時間: 2025-4-1 19:44 作者: 牢騷 時間: 2025-4-1 22:51 作者: Creditee 時間: 2025-4-2 05:42 作者: facetious 時間: 2025-4-2 10:28
