標(biāo)題: Titlebook: Engineering Applications of Computational Fluid Dynamics; Ku Zilati Ku Shaari,Mokhtar Awang Book 2015 Springer International Publishing Sw [打印本頁] 作者: 女孩 時間: 2025-3-21 18:27
書目名稱Engineering Applications of Computational Fluid Dynamics影響因子(影響力)
書目名稱Engineering Applications of Computational Fluid Dynamics影響因子(影響力)學(xué)科排名
書目名稱Engineering Applications of Computational Fluid Dynamics網(wǎng)絡(luò)公開度
書目名稱Engineering Applications of Computational Fluid Dynamics網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Engineering Applications of Computational Fluid Dynamics被引頻次
書目名稱Engineering Applications of Computational Fluid Dynamics被引頻次學(xué)科排名
書目名稱Engineering Applications of Computational Fluid Dynamics年度引用
書目名稱Engineering Applications of Computational Fluid Dynamics年度引用學(xué)科排名
書目名稱Engineering Applications of Computational Fluid Dynamics讀者反饋
書目名稱Engineering Applications of Computational Fluid Dynamics讀者反饋學(xué)科排名
作者: 珍奇 時間: 2025-3-21 22:53 作者: 調(diào)整校對 時間: 2025-3-22 02:06 作者: 哎呦 時間: 2025-3-22 07:16
Localization of Rotating Sound Sources Using Time Domain Beamforming Code,Some applications in acoustics involve rotating sound sources around a fixed axis in space. For example, the noise emitted by fans is of interest and because of the fast rotation, the sound sources are not easy to locate with the standard delay-and-sum beamforming code. In the time domain approach f作者: 束縛 時間: 2025-3-22 09:11
Effects of the Surrounding Fluid on the Dynamic Characteristics of Circular Plates,rounded by a fluid of low density has been studied. Thus, it has been shown that the air effect for the Intelsat VI C–B transmit reflector with a diameter of 3.2?m and weighting only 34.7?kg decreases the first modal frequency by 20?% with respect to the value in vacuum. It is important then, in the作者: Deceit 時間: 2025-3-22 16:31
CFD Modelling of the Coanda Based Thrust Vectoring Nozzle,de a directional thrust without any movement of mechanical parts, by utilizing the Coanda effect to divert a jet from the symmetry axis. The deviation of the jet produces an oriented thrust vector due to the existence of a perpendicular component to the main propulsive direction. The studied nozzle 作者: Deceit 時間: 2025-3-22 20:42
Numerical Investigation of the Flow Over Delta Wing and Reverse Delta Wing,hich are delta wing (DW) and reverse delta wing (RDW). However, as a preliminary investigation, the study has treated these devices separately from the aircraft in order to clearly visualize the wake vortex formation behind the wing as a standalone. Simulations were performed using RANS turbulence m作者: VERT 時間: 2025-3-22 23:12 作者: 胖人手藝好 時間: 2025-3-23 03:46
Unsteady Interaction Effects Between an Airship and Its Air-Jet Propulsion System,for Transportation. The airship has a cylindrical shape when completely inflated at the pressure altitude. Based on an initial research for the airship shape and aerodynamic features at given altitudes, propulsion needs were analyzed by means of numerical simulations for different flow conditions an作者: Generalize 時間: 2025-3-23 08:45
Numerical Investigation on the Nanofluid Flow and Heat Transfer in a Wavy Channel, governing continuity, momentum and energy equations in body-fitted coordinates are discretized using finite volume approach and solved iteratively using SIMPLE algorithm. The study covers Reynolds number and nanoparticle volume concentration in the ranges of 100–800 and 0–5?% respectively. The effe作者: 不確定 時間: 2025-3-23 12:17
Book 2015This volume presents the results of Computational Fluid Dynamics (CFD) analysis that can be used for conceptual studies of product design, detail product development, process troubleshooting. It demonstrates the benefit of CFD modeling as a cost saving, timely, safe and easy to scale-up methodology.作者: cliche 時間: 2025-3-23 14:25
https://doi.org/10.1007/978-3-319-02836-1Beamforming Code; Biomass Gasification Reaction; Fluid-structure Interaction; Hydrodynamics; Large Eddy 作者: SHOCK 時間: 2025-3-23 21:46
978-3-319-35027-1Springer International Publishing Switzerland 2015作者: 歪曲道理 時間: 2025-3-24 01:27
Engineering Applications of Computational Fluid Dynamics978-3-319-02836-1Series ISSN 1869-8433 Series E-ISSN 1869-8441 作者: BURSA 時間: 2025-3-24 03:49 作者: 就職 時間: 2025-3-24 08:05 作者: 蒙太奇 時間: 2025-3-24 11:12 作者: Yourself 時間: 2025-3-24 16:02 作者: miscreant 時間: 2025-3-24 22:25 作者: 編輯才信任 時間: 2025-3-25 00:40
https://doi.org/10.1007/978-3-642-65584-5de a directional thrust without any movement of mechanical parts, by utilizing the Coanda effect to divert a jet from the symmetry axis. The deviation of the jet produces an oriented thrust vector due to the existence of a perpendicular component to the main propulsive direction. The studied nozzle 作者: Palate 時間: 2025-3-25 03:41
https://doi.org/10.1007/978-3-642-94633-2hich are delta wing (DW) and reverse delta wing (RDW). However, as a preliminary investigation, the study has treated these devices separately from the aircraft in order to clearly visualize the wake vortex formation behind the wing as a standalone. Simulations were performed using RANS turbulence m作者: Biguanides 時間: 2025-3-25 10:54 作者: 集聚成團(tuán) 時間: 2025-3-25 13:09 作者: 使熄滅 時間: 2025-3-25 18:43
Taschenbuch der Mathematik und Physik governing continuity, momentum and energy equations in body-fitted coordinates are discretized using finite volume approach and solved iteratively using SIMPLE algorithm. The study covers Reynolds number and nanoparticle volume concentration in the ranges of 100–800 and 0–5?% respectively. The effe作者: mettlesome 時間: 2025-3-25 21:59
Ku Zilati Ku Shaari,Mokhtar AwangPresents the results of CFD analysis that can be used for conceptual studies of product design, detail product development, process troubleshooting.Demonstrates the benefit of CFD modeling as a cost s作者: FADE 時間: 2025-3-26 01:25 作者: obsolete 時間: 2025-3-26 06:57 作者: Biguanides 時間: 2025-3-26 11:35 作者: 機(jī)警 時間: 2025-3-26 15:30 作者: airborne 時間: 2025-3-26 19:46 作者: Cupping 時間: 2025-3-26 23:49
Numerical Modeling and Research of 3D Turbine Stage,hed. The elaborated methodology was applied for research of boundary layer development; radial gap effects on flow aerodynamics in turbine stages; erosion effects over turbine blades working in wet steam; roughness influence over turbine blade surface, etc.作者: 枕墊 時間: 2025-3-27 04:23
Taschenbuch der Hochfrequenztechnik three dimensional cavity flows agrees well with those documented by previous investigators. It has been shown here that the Lattice Boltzmann method is an effective computational fluid dynamics tool to study high Re flows.作者: 廣告 時間: 2025-3-27 05:52
Taschenbuch der Mathematik und Physikenhancement in heat transfer by addition of nanoparticles. This enhancement increase with concentration of particles but the required pumping power also increases. The present results display a good agreement with the literature.作者: 服從 時間: 2025-3-27 13:10 作者: Cabinet 時間: 2025-3-27 15:12
Numerical Investigation on the Nanofluid Flow and Heat Transfer in a Wavy Channel,enhancement in heat transfer by addition of nanoparticles. This enhancement increase with concentration of particles but the required pumping power also increases. The present results display a good agreement with the literature.作者: 刺耳的聲音 時間: 2025-3-27 20:52
Reaction Modeling for Prediction of Hydrogen Production During Biomass Gasification, to biomass ratio) for the production of hydrogen. In this work, the hydrodynamic and reaction models were developed concurrently. The reaction model which was empirically validated was developed and implemented using ANSYS Fluent. V6.3. Some comparative analyses were carried out between the simulated and experimental results.作者: 攤位 時間: 2025-3-27 22:38 作者: AVERT 時間: 2025-3-28 03:13 作者: 象形文字 時間: 2025-3-28 08:45 作者: motivate 時間: 2025-3-28 13:15 作者: Outspoken 時間: 2025-3-28 15:30
https://doi.org/10.1007/978-3-642-65584-5 In particular, the dependency of the thrust change in respect to the inlet conditions is analysed for different scenarios, with special focus on the thrust magnitude and its direction. The following parameters affecting the flow field of the nozzle have been studied: (a) the ratio of inlet velociti作者: Biomarker 時間: 2025-3-28 19:43
https://doi.org/10.1007/978-3-642-94633-2e size of the vortex is not predicted correctly by RANS turbulence model. Overall, it can be concluded from the results that the wake vortex generated from DW exhibit higher tangential velocity magnitude and circulation than the one generated from RDW at a particular angle of attack (AOA) between 20作者: 別炫耀 時間: 2025-3-29 01:09
,Physikalische Gr??en und Konstanten,urther enhanced by computing the near vehicle flow when it is subject to the incoming wind. We will also present details about the total required thrust power for the various working conditions. The outcome of the research highlights the main advantages of the system to attain feasible high altitude作者: Delectable 時間: 2025-3-29 05:20
Localization of Rotating Sound Sources Using Time Domain Beamforming Code,dent delay due to the time dependent distance .(.). In contrast to the standard beamforming code, this time domain beamforming code allows to treat rotating sound sources as well as stationary sound sources. In this chapter the differences between the standard delay-and-sum beamforming to the rotati
