Fatigue Test

Validation of Analysis through Detailed or Whole Aircraft Testing

Fatigue Test
  • Specimen description and modification standard, instrumentation and data recording requirements, loads to be applied, specimen constraints, test aims and pass/fail criteria
  • Calculation of expected strain gauge responses
  • Definition of inspection requirements, allowable damage, Go/No Go criteria
  • Test interpretation, significance of defects, comparison with theoretical performance (crack initiation and propagation), determination of certification compliance demonstrated

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+44(0)1292 67 5245