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

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发表于 2025-3-28 15:30:36 | 显示全部楼层
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
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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
发表于 2025-3-29 01:09:44 | 显示全部楼层
,Physikalische Größen 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
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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
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