Titlebook: ICAF 2009, Bridging the Gap between Theory and Operational Practice; Proceedings of the 2 M. J. Bos Conference proceedings 2009 Springer Sc

使閉塞

外露

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

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

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

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

Gene408

Fracture

CRANK

CHIP