Adams
发表于 2025-3-21 18:57:56
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Mercantile
发表于 2025-3-21 21:17:45
2191-530X -safe and damage tolerance approaches, allowing weight savings and increasing aircraft reliability and structural integrity..The application of the damage tolerance approach requires extensive know-how of the fatigue and fracture properties, corrosion strength, potential failure modes and non-destru
Rodent
发表于 2025-3-22 03:08:08
Book 2019rom basic mode I evaluations using rough finite element approaches, to current 3D modeling based on energetic approaches as the VCCT, or simulation of joining processes. This book provides a concise introduction to this subject..
破布
发表于 2025-3-22 07:10:18
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nepotism
发表于 2025-3-22 09:28:14
Introductionf mechanical components in his laboratory, mentions an even greater percentage attributable to fatigue, see Table 1.1, from Nishida (Failure analysis in engineering applications. Butterworth-Heinemann, 1992.)
托人看管
发表于 2025-3-22 13:19:13
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托人看管
发表于 2025-3-22 21:00:21
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Commonwealth
发表于 2025-3-22 22:03:44
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BORE
发表于 2025-3-23 03:13:13
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表示问
发表于 2025-3-23 06:30:18
Sérgio M. O. Tavares,Paulo M. S. T. de CastroProvides a state-of-the-art review of the fail-safe and damage tolerance approaches