使闭塞
发表于 2025-3-23 12:10:13
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外露
发表于 2025-3-23 15:40:23
Concept Of The New A320 Fatigue Testysis/justification for an extension of the limit of validity (LoV) of the maintenance program to ensure continuation of safe aircraft operation. Up to 180,000 SF have to be performed to simulate the fatigue and damage tolerance behaviour of the airframe. The concepts of the new fatigue tests have be
投射
发表于 2025-3-23 20:54:30
The Use Of Composite Material Strips To Extend The Damage-Tolerance Life Of Integrally Stiffened Aluesting was performed at room-temperature and at −50°C. The test results identify a large potential for increasing significantly the damage-tolerance life of these panels. The analytical results, based on finite-element models, correlate very well with the test results.
Concerto
发表于 2025-3-24 01:23:38
Structural Integrity Of A Wing Upper Skin With Exfoliation Corrosion skin. Finite element and fatigue strength analyses were carried out to quantify the impact of exfoliation corrosion and grind-out repairs at fastener holes on a wing upper skin under a fighter aircraft spectrum loading. The analytical models were compared and validated by test results. The tests we
魅力
发表于 2025-3-24 05:13:32
Helicopter Structural Integrity Program Of Polish Mi-24 Hind Helicoptersen presented. In the paper abilities of IT system, the SAMANTA system used in Polish Armed Forces for collecting and analysing operational and maintenance related information have been discussed. Advantages from application of relational data base technology implemented in the SAMANTA system and bas
CAMP
发表于 2025-3-24 08:24:50
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Gene408
发表于 2025-3-24 12:06:36
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Fracture
发表于 2025-3-24 16:01:43
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CRANK
发表于 2025-3-24 20:42:37
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CHIP
发表于 2025-3-25 00:01:54
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