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標(biāo)題: Titlebook: Direct and Large Eddy Simulation XIII; Proceedings of DLES1 Cristian Marchioli,Maria Vittoria Salvetti,Philipp Conference proceedings 2024 [打印本頁]

作者: notable    時(shí)間: 2025-3-21 16:35
書目名稱Direct and Large Eddy Simulation XIII影響因子(影響力)




書目名稱Direct and Large Eddy Simulation XIII影響因子(影響力)學(xué)科排名




書目名稱Direct and Large Eddy Simulation XIII網(wǎng)絡(luò)公開度




書目名稱Direct and Large Eddy Simulation XIII網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Direct and Large Eddy Simulation XIII被引頻次




書目名稱Direct and Large Eddy Simulation XIII被引頻次學(xué)科排名




書目名稱Direct and Large Eddy Simulation XIII年度引用




書目名稱Direct and Large Eddy Simulation XIII年度引用學(xué)科排名




書目名稱Direct and Large Eddy Simulation XIII讀者反饋




書目名稱Direct and Large Eddy Simulation XIII讀者反饋學(xué)科排名





作者: Bph773    時(shí)間: 2025-3-21 20:14

作者: 割公牛膨脹    時(shí)間: 2025-3-22 02:55
Large-Eddy Simulations of?the?Accelerating Flow Around a?Square Cylindernterest for wind-engineering applications, typical, e.g., of skyscrapers and towers. Despite the simple geometry, the flow features around square cylinders or prisms show a significant complexity. In particular, the flow is characterized by the shear-layer separation at the upstream edges. The separ
作者: Nebulizer    時(shí)間: 2025-3-22 08:09
DNS and?POD Analysis of?Separated Flow in?a?Three-Dimensional Diffusernumerical and experimental data, even without smoothing of the sharp corners. Discrepancies in the duct area have been found to be due to uncertainties, however, in the diffuser region differences are more noticeably between experimental and numerical data, where they all exhibit an oscillating beha
作者: 戰(zhàn)役    時(shí)間: 2025-3-22 12:20

作者: Capture    時(shí)間: 2025-3-22 13:14
Euler-Lagrange LES Predictions of?a?Powder Disperser Including a?Multiscale Wall-Impact Breakage Mode.g., air pollution) and industrial applications (e.g., dry powder inhalers). The main challenge for investigating such flows is the extensive range of length and time scales to be dealt with, especially in the case of turbulent flows.
作者: Capture    時(shí)間: 2025-3-22 19:50

作者: 挑剔小責(zé)    時(shí)間: 2025-3-22 21:26

作者: Vertebra    時(shí)間: 2025-3-23 05:02
Dynamics of?Turbulent Kinetic Energy Advection in?a?Turbulent Boundary Layer Under Unsteady Pressure from the medical field, to engineering applications, to the natural sciences. In most of the practical applications the pressure gradient varies both spatially and temporally giving rise to a transient separation process often associated with a drop in performance of many systems (e.g. wings, turbomachinery).
作者: 寵愛    時(shí)間: 2025-3-23 05:34
In-Situ Analysis of?Backflow Events and?Their Relation to?Separation in?Wings Through Well-Resolved ed to pressure gradients (PGs). The presence of such PGs affects greatly the development and physics of the turbulent boundary layer (TBL), making it an open research area. An important phenomena associated with the presence of strong adverse PGs (APGs) as appearing in wings, is the separation of the boundary layer, which can lead to stall.
作者: ordain    時(shí)間: 2025-3-23 10:03
Euler-Lagrange LES Predictions of?a?Powder Disperser Including a?Multiscale Wall-Impact Breakage Mode.g., air pollution) and industrial applications (e.g., dry powder inhalers). The main challenge for investigating such flows is the extensive range of length and time scales to be dealt with, especially in the case of turbulent flows.
作者: 浸軟    時(shí)間: 2025-3-23 16:00
Mack Breazeale Ph.D.,Michael McPherson from the medical field, to engineering applications, to the natural sciences. In most of the practical applications the pressure gradient varies both spatially and temporally giving rise to a transient separation process often associated with a drop in performance of many systems (e.g. wings, turbo
作者: 牲畜欄    時(shí)間: 2025-3-23 21:17
Mack A. Breazeale,Michael McPhersoned to pressure gradients (PGs). The presence of such PGs affects greatly the development and physics of the turbulent boundary layer (TBL), making it an open research area. An important phenomena associated with the presence of strong adverse PGs (APGs) as appearing in wings, is the separation of th
作者: 友好    時(shí)間: 2025-3-23 22:20

作者: curriculum    時(shí)間: 2025-3-24 02:38
Sound Propagation in the Atmospherenumerical and experimental data, even without smoothing of the sharp corners. Discrepancies in the duct area have been found to be due to uncertainties, however, in the diffuser region differences are more noticeably between experimental and numerical data, where they all exhibit an oscillating beha
作者: Grasping    時(shí)間: 2025-3-24 09:15

作者: ALOFT    時(shí)間: 2025-3-24 12:37

作者: 喧鬧    時(shí)間: 2025-3-24 16:30
https://doi.org/10.1007/978-3-030-52171-4 However, coal is considered an environmentally harmful fuel that releases large amounts of greenhouse gases and pollutants during firing. Measures must therefore be taken to improve Pulverized Coal Combustion (PCC) and reduce emissions. Numerical simulations have become increasingly important for t
作者: JIBE    時(shí)間: 2025-3-24 20:26
https://doi.org/10.1007/978-0-387-26308-3.6, both based on isentropic exit conditions, using a high order discontinuous Galerkin method. The aim is to validate the numerical setup with respect to available experimental data. We discuss the steps taken to create realistic inflow boundary conditions in terms of end wall boundary layer thickn
作者: 四目在模仿    時(shí)間: 2025-3-24 23:42

作者: 螢火蟲    時(shí)間: 2025-3-25 06:31
ERCOFTAC Serieshttp://image.papertrans.cn/e/image/280640.jpg
作者: 向前變橢圓    時(shí)間: 2025-3-25 10:25

作者: 噴出    時(shí)間: 2025-3-25 14:01
Christoph Klahn,Bastian Leutenecker-TwelsiekVariable density flows are very common in nature, in technology and in industry. The numerical simulation of complex flows of applicative interest and with relevant variable density flows requires the truncation of turbulent scales of the resolved velocity field, in order to reduce the required computational resources.
作者: 熄滅    時(shí)間: 2025-3-25 17:04
Identification of Suitable PartsMass transfer in bubbly flows is ubiquitous in nature and industry. For instance, bubble chemical reactors and mass-transfer operations of chemical engineering (e.g., distillation columns) employ bubbly flows to produce chemical products or to promote separation processes.
作者: CHART    時(shí)間: 2025-3-25 22:00
Verena Pramhaas,Günther RupprechterThe ISIS Muon and Neutron source uses the spallation of protons accelerated to 84?% of the speed of light to generate neutrons at two tungsten targets clad in tantalum and cooled by recirculating water.
作者: 用手捏    時(shí)間: 2025-3-26 00:15

作者: genesis    時(shí)間: 2025-3-26 07:15

作者: neoplasm    時(shí)間: 2025-3-26 11:56

作者: 預(yù)定    時(shí)間: 2025-3-26 16:00
DNS of?the?Flow About a?5:1 Rectangular Body with?Sharp CornersThe turbulent flow about blunt, rectangular bodies is often encountered in civil and wind engineering applications as well as in land transport vehicles. Relevant examples include deck slabs of long-span bridges and high-rise buildings of rectangular section and the problem of the aerodynamics of vehicles of simple shape like trucks and trains.
作者: obstinate    時(shí)間: 2025-3-26 18:44
Effect of?Variable Density on?Subgrid ScalesVariable density flows are very common in nature, in technology and in industry. The numerical simulation of complex flows of applicative interest and with relevant variable density flows requires the truncation of turbulent scales of the resolved velocity field, in order to reduce the required computational resources.
作者: Spirometry    時(shí)間: 2025-3-26 22:02

作者: Eeg332    時(shí)間: 2025-3-27 03:10
Application of?LES to?the?Thermal–Hydraulics of?Target Station 2 of?the?ISIS Muon and?Neutron SourceThe ISIS Muon and Neutron source uses the spallation of protons accelerated to 84?% of the speed of light to generate neutrons at two tungsten targets clad in tantalum and cooled by recirculating water.
作者: 滑稽    時(shí)間: 2025-3-27 08:36

作者: Palpitation    時(shí)間: 2025-3-27 09:27

作者: 是剝皮    時(shí)間: 2025-3-27 13:38
Wind Gust-Induced Flutter of?an?Elastically Mounted Airfoil: A Fluid-Structure Interaction Study BasClassical investigations on the aeroelasticity of wings used for the analysis of flutter stability are often carried out based on simplifying model configurations given by elastically mounted rigid wings.
作者: 停止償付    時(shí)間: 2025-3-27 17:48
https://doi.org/10.1007/978-3-031-47028-8Fluid Dynamics; Turbulence; Direct Numerical Simulation; Large-Eddy Simulation; LES Modelling; DLES
作者: 來自于    時(shí)間: 2025-3-27 23:13
978-3-031-47030-1The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl
作者: 熱情的我    時(shí)間: 2025-3-28 04:48
Direct and Large Eddy Simulation XIII978-3-031-47028-8Series ISSN 1382-4309 Series E-ISSN 2215-1826
作者: 過時(shí)    時(shí)間: 2025-3-28 06:51
Mack Breazeale Ph.D.,Michael McPherson from the medical field, to engineering applications, to the natural sciences. In most of the practical applications the pressure gradient varies both spatially and temporally giving rise to a transient separation process often associated with a drop in performance of many systems (e.g. wings, turbomachinery).
作者: Expand    時(shí)間: 2025-3-28 12:25
Mack A. Breazeale,Michael McPhersoned to pressure gradients (PGs). The presence of such PGs affects greatly the development and physics of the turbulent boundary layer (TBL), making it an open research area. An important phenomena associated with the presence of strong adverse PGs (APGs) as appearing in wings, is the separation of the boundary layer, which can lead to stall.
作者: maladorit    時(shí)間: 2025-3-28 16:10

作者: Manifest    時(shí)間: 2025-3-28 21:46
Large-Eddy Simulations of?the?Flow Around Rectangular Cylinders of?Different Chord-to-Depth Ratios:
作者: CRAB    時(shí)間: 2025-3-29 00:46
1382-4309 ss transport phenomena. The sixth section covers Data Assimilation and Uncertainty Quantification, featuring two papers that highlight the importance of incorporating data into fluid dynamic models and quantify978-3-031-47030-1978-3-031-47028-8Series ISSN 1382-4309 Series E-ISSN 2215-1826
作者: Interim    時(shí)間: 2025-3-29 06:49
Conference proceedings 2024luid flows, addressing topics such as convective heat transfer, natural convection, and mass transport phenomena. The sixth section covers Data Assimilation and Uncertainty Quantification, featuring two papers that highlight the importance of incorporating data into fluid dynamic models and quantify
作者: Paradox    時(shí)間: 2025-3-29 09:18
1382-4309 n the most relevant special topics concerning Direct and Lar.This book covers the diverse and cutting-edge research presented at the 13th ERCOFTAC Workshop on Direct and Large Eddy Simulation. The first section of the book focuses on Aerodynamics/Aeroacoustics, comprising eight papers that delve int
作者: 加花粗鄙人    時(shí)間: 2025-3-29 13:52

作者: Custodian    時(shí)間: 2025-3-29 19:21
https://doi.org/10.1007/978-3-030-52171-4he detailed understanding of PCC in recent years. Combustion models for gaseous combustion were extended to describe PCC. Among these models, the flamelet model (Peters, .) has proven to be a precise model that can represent detailed chemical mechanisms with low computational effort.
作者: 材料等    時(shí)間: 2025-3-29 21:59

作者: Preamble    時(shí)間: 2025-3-29 23:59
https://doi.org/10.1007/978-0-387-26308-3nts. Following a short discussion of the secondary flow structures emerging due to the interaction of the incoming boundary layer and the turbine blade, we show that this simulation is also able to reproduce loss distribution behind the blade over the whole channel height.
作者: 厚顏    時(shí)間: 2025-3-30 05:01
DNS and?POD Analysis of?Separated Flow in?a?Three-Dimensional Diffuserto be the main reason of discrepancy between all datasets. While DNS of turbulent flow at . are feasible nowadays, temporal dynamics of the Standford diffuser present a challenge as the integration time needed becomes larger. The current dataset is, nevertheless, valid for further analysis and activities and will be made available online.
作者: generic    時(shí)間: 2025-3-30 10:15
Large Eddy Simulation of?a?Low Pressure Turbine Cascade with?Turbulent End Wall Boundary Layersnts. Following a short discussion of the secondary flow structures emerging due to the interaction of the incoming boundary layer and the turbine blade, we show that this simulation is also able to reproduce loss distribution behind the blade over the whole channel height.
作者: 明確    時(shí)間: 2025-3-30 14:04
Conference proceedings 2024 of the book focuses on Aerodynamics/Aeroacoustics, comprising eight papers that delve into the intricate relationship between fluid flow and aerodynamic performance. The second section explores the dynamics of Bluff/Moving Bodies through four insightful papers. Bubbly Flows, the subject of the thir
作者: 油氈    時(shí)間: 2025-3-30 19:09
Large-Eddy Simulations of?the?Accelerating Flow Around a?Square Cylinderated shear layers undergo to Kelvin-Helmholtz instability, but they do not lose coherence until they form the von Karman vortex street in the wake. In terms of mean flow features, no reattachment is found on the lateral surface of the cylinder.
作者: 平躺    時(shí)間: 2025-3-31 00:26

作者: Flagging    時(shí)間: 2025-3-31 03:38

作者: 五行打油詩    時(shí)間: 2025-3-31 07:17

作者: tic-douloureux    時(shí)間: 2025-3-31 11:00





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