BLANC
发表于 2025-3-23 12:41:11
Marilisa Botte,Luca D’Acierno,Mariano Gallomount of abnormality/fault leads to catastrophic failure of critical components (e.g., bearing, coupling, rotor, gearbox, etc.) in turbo generator systems. The catastrophic failure of these critical component results huge economic loss sometimes even worse loss of human life to the firm. Two flexibl
floodgate
发表于 2025-3-23 17:18:39
Marilisa Botte,Luca D’Acierno,Mariano Gallong phenomena between bending and lateral vibration due to the presence of crack is used for the identification of crack in an overhung rotor system. The natural frequency of the rotor system has been obtained using impact hammer analysis and compared with the finite element analysis. The crack ident
原始
发表于 2025-3-23 20:34:54
Towards a Resident Static Analysisrchers have calculated SIFs in a cracked beam or rotor made of homogeneous materials, but for functionally graded (FG) materials is scarce. The radially graded FG shaft consists of aluminum oxide (Al.O.) as ceramic constituent and stainless steel (SS) is as metal constituent and properties of materi
doxazosin
发表于 2025-3-23 22:22:15
Giulia Datola,Marta Bottero,Elena De Angelismeters, namely amount of the damage intensity and location. This approach of identification is established by integrating the response surface methodology (RSM) and genetic algorithm (GA). Numerical finite element (FE) model of the cracked beam has been connected to the present approach to carry out
embolus
发表于 2025-3-24 02:39:03
Valery G. Gitis,Alexander B. Derendyaevping system. The failure prediction is done by choosing limits on ratcheting and fatigue usage factor. Strain accumulation in the system is predicted using the numerical method. In this method, ratcheting in the piping loop is evaluated by carrying out response spectrum analysis at system level usin
考得
发表于 2025-3-24 07:48:51
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Baffle
发表于 2025-3-24 13:54:18
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混沌
发表于 2025-3-24 14:58:09
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vitrectomy
发表于 2025-3-24 22:27:00
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Fecal-Impaction
发表于 2025-3-25 02:35:22
https://doi.org/10.1007/978-981-15-5693-7Structural vibration; Aerospace Structures; Vehicle dynamics; Fluid structure interaction; Rotor dynamic