Effect of Fatigue and Damage Tolerance Material Properties on the Efficiency of Aircraft Structures

  1. Hasso Weiland,
  2. Anthony D. Rollett and
  3. William A. Cassada
  1. Hans-Juergen Schmidt and
  2. Bianka Schmidt-Brandecker

Published Online: 4 SEP 2012

DOI: 10.1002/9781118495292.ch67

ICAA13: 13th International Conference on Aluminum Alloys

ICAA13: 13th International Conference on Aluminum Alloys

How to Cite

Schmidt, H.-J. and Schmidt-Brandecker, B. (2012) Effect of Fatigue and Damage Tolerance Material Properties on the Efficiency of Aircraft Structures, in ICAA13: 13th International Conference on Aluminum Alloys (eds H. Weiland, A. D. Rollett and W. A. Cassada), John Wiley & Sons, Inc., Hoboken, NJ, USA. doi: 10.1002/9781118495292.ch67

Publication History

  1. Published Online: 4 SEP 2012
  2. Published Print: 5 JUN 2012

ISBN Information

Print ISBN: 9781118458044

Online ISBN: 9781118495292

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Keywords:

  • Fatigue;
  • Damage Tolerance;
  • Materials;
  • Structure

Summary

This chapter contains sections titled:

  • Introduction

  • Damage Tolerance Concept

  • Opportunities to Increase the Efficiency of Aircraft Structure

  • Allowable Stresses to Meet Required Inspection Intervals and Two-Bay-Crack Criterion

  • Conclusion