Statistical estimation of economic life for aircraft structures

This publication has 11 references indexed in Scilit:

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• New Air Force Requirements for Structural Safety, Durability, and Life Management
  Journal of Aircraft, 1976
• Current Practice on Estimating Crack Growth Damage Accumulation with Specific Application to Structural Safety Durability and Reliability
  Published by Defense Technical Information Center (DTIC) ,1976
• Inspection frequency optimization for aircraft structures based on reliability analysis
  Journal of Aircraft, 1975
• Reliability After Inspection
  Published by ASTM International ,1975
• Methods for analyzing fatigue crack growth rate behavior associated with flight-by-flight loading
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1974
• Method of analysis and prediction for variable amplitude fatigue crack growth
  Engineering Fracture Mechanics, 1972
• Development of Titanium and Steel Fatigue Variability Model for Application of Reliability Analysis Approach to Aircraft Structures
  Published by Defense Technical Information Center (DTIC) ,1972
• Cracks, A FORTRAN IV Digital Computer Program for Crack Propagation Analysis
  Published by Defense Technical Information Center (DTIC) ,1970
• RELIABILITY ANALYSIS BASED ON TIME TO FIRST FAILURE
  Published by Defense Technical Information Center (DTIC) ,1967