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Titlebook: Advances in Mechanical Engineering and Technology; Proceedings of 6th I Ranganath M. Singari,Pavan Kumar Kankar,Girija Moo Conference proce

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樓主: Diverticulum
41#
發(fā)表于 2025-3-28 15:30:07 | 只看該作者
42#
發(fā)表于 2025-3-28 22:35:34 | 只看該作者
The Study of Verbs in Cognitive Scienceed out in Ansys FLUENT, which solves three-dimensional Navier–Stokes and energy equations. Lubricant flow has been considered as laminar. Thermal effects and hydrodynamic pressure of the fluid film of circular journal bearing are studied by varying viscosity index in the range of 0.75–1.3. Clearance
43#
發(fā)表于 2025-3-28 23:51:09 | 只看該作者
https://doi.org/10.1007/978-3-319-10112-5ilizing molded instruments, tall-recurrence mechanical movement, then a rough slurry. Ultrasonic machining (USM) boundaries (like slurry fixation, force, and feed rate) on material evacuation rate, tighten point during zirconia machining, and over-cut (ZrO.) composite. The investigations are led bas
44#
發(fā)表于 2025-3-29 07:01:07 | 只看該作者
45#
發(fā)表于 2025-3-29 09:19:16 | 只看該作者
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發(fā)表于 2025-3-29 13:12:47 | 只看該作者
47#
發(fā)表于 2025-3-29 19:24:39 | 只看該作者
48#
發(fā)表于 2025-3-29 22:37:15 | 只看該作者
https://doi.org/10.1007/978-3-319-10112-5he stimulated pollination by means of nano copters or small drones to increase productivity in the field of agriculture employing of automated or manual control. Therefore, a robust design can be made by change in its structure or modification in its programming system with respect to its flight con
49#
發(fā)表于 2025-3-30 02:52:06 | 只看該作者
The Study of Verbs in Cognitive Sciencee by the use of YOLOv3 model.?The model was used to train a dataset of 12,000 images which consisted of the images of both biodegradable and?non-biodegradable wastes and the MAP efficiency of the model was 99.57% to detect the images which makes it a?fairly accurate model to be used for the classifi
50#
發(fā)表于 2025-3-30 04:57:47 | 只看該作者
https://doi.org/10.1007/978-3-319-10112-5art off and landing, however, these properties of delta wing conjointly depend on lift, drag, attack angle, velocity, sound impact absorption, thermal conditions and plenty more properties, which directly make the change in performance of aircraft vary. This paper examines the vortex flow over the c
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