Titlebook: Engineering Applications of Computational Fluid Dynamics; Ku Zilati Ku Shaari,Mokhtar Awang Book 2015 Springer International Publishing Sw

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书目名称Engineering Applications of Computational Fluid Dynamics影响因子(影响力)




书目名称Engineering Applications of Computational Fluid Dynamics影响因子(影响力)学科排名




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书目名称Engineering Applications of Computational Fluid Dynamics网络公开度学科排名




书目名称Engineering Applications of Computational Fluid Dynamics被引频次




书目名称Engineering Applications of Computational Fluid Dynamics被引频次学科排名




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书目名称Engineering Applications of Computational Fluid Dynamics年度引用学科排名




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书目名称Engineering Applications of Computational Fluid Dynamics读者反馈学科排名

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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

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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

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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

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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

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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

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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