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CEAS Forum~Life Extension~Aerospace Technology Opportunities
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The contribution of fatigue usage monitoring systems to life extension in safe-life and damage-tolerant designs

  • Technical Paper
  • 1999-11-0023
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Derived criteria for updating aircraft fatigue life predictions

  • Technical Paper
  • 1999-11-0025
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Improving the fatigue crack resistance of 2024-T351 aluminum alloy by shot peening

  • Technical Paper
  • 1999-11-0029
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

The meaning of life

  • Technical Paper
  • 1999-11-0027
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Airbus A300 extended operational limits~Opportunities and a proposed means of wing structure justification

  • Technical Paper
  • 1999-11-0010
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Keynote Address: Effect of multiple-site-damage on certified lead crack residual strength

  • Technical Paper
  • 1999-11-0008
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Experience on airbus full-scale fatigue tests with respect to life extension

  • Technical Paper
  • 1999-11-0012
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Continued structural integrity for the RAF VC10

  • Technical Paper
  • 1999-11-0014
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Tornado life extension program

  • Technical Paper
  • 1999-11-0016
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom

Olympus Non-Advocate Review

  • Technical Paper
  • 1999-11-0020
Published 1999-03-23 by Royal Aeronautical Society in United Kingdom