Damage Tolerance Applied to the Design of Mid-Size Aircraft

  1. Hasso Weiland,
  2. Anthony D. Rollett and
  3. William A. Cassada
  1. Carlos Eduardo Chaves

Published Online: 4 SEP 2012

DOI: 10.1002/9781118495292.ch84

ICAA13: 13th International Conference on Aluminum Alloys

ICAA13: 13th International Conference on Aluminum Alloys

How to Cite

Chaves, C. E. (2012) Damage Tolerance Applied to the Design of Mid-Size Aircraft, 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.ch84

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:

  • damage tolerance;
  • fatigue;
  • mid-size aircraft

Summary

This chapter contains sections titled:

  • Introduction

  • Fatigue and Damage Tolerance Evaluation of Metallic Structures

  • Fatigue and Damage Tolerance Evaluation of Composite Structures

  • Future Trends and Perspectives

  • Conclusions