Aircraft Fatigue
eBook - PDF

Aircraft Fatigue

Design, Operational and Economic Aspects

  1. 572 pages
  2. English
  3. PDF
  4. Only available on web
eBook - PDF

Aircraft Fatigue

Design, Operational and Economic Aspects

Book details
Table of contents
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About This Book

Aircraft Fatigue: Design, Operational and Economic Aspects contains the proceedings of the ""Symposium on Aircraft Fatigue—Design, Operational and Economic Aspects, "" held in Melbourne, Australia, on May 22-24, 1967. The papers explore the design and operational aspects of the fatigue problem in general aviation and transport aircraft, as well as the economic aspects of the fatigue problem as it affects both operators and manufacturers. This book is comprised of 21 chapters and begins with a description of an approach to structural reliability analysis based on order statistics and the expected time to first failure in a fleet of specified magnitude, along with its application to structures subject to progressive fatigue damage. The following chapters deal with structural load measurement and analysis; design and certification programs for a wide range of aircraft types including the Anglo-French and American civil supersonic transports; acoustic fatigue; and the design of joints. The detection of fatigue cracks in service and the effects of fatigue on the cost of design and operation of aircraft are also discussed. This monograph will be a useful resource for aircraft and aeronautical engineers as well as officials of civil aviation.

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Information

Publisher
Pergamon
Year
2013
ISBN
9781483146454
Topic
Business
Subtopic
Transportation Industry
Index
Business

Table of contents

  1. Front Cover
  2. Aircraft Fatigue: Design, Operational and Economic Aspects
  3. Copyright Page
  4. Table of Contnets
  5. Dedication
  6. PREFACE
  7. SESSION CHAIRMEN
  8. AUSTRALIAN ORGANISING COMMITTEE
  9. ABBREVIATIONS
  10. THE INTERNATIONAL COMMITTEE ON AERO-NAUTICAL FATIGUE (ICAF) ITS FOUNDATION, GROWTH AND TODAY'S PHILOSOPHY
  11. CHAPTER 1. RELIABILITY ANALYSIS BASED ON TIME TO THE FIRST FAILURE
  12. CHAPTER 2. OPTIMUM DESIGN OF JOINTS: THE STRESS SEVERITY FACTOR CONCEPT
  13. CHAPTER 3. FATIGUE TESTING OF THE F.28 FELLOWSHIP
  14. CHAPTER 4. DESIGN AND CERTIFICATION FOR EXECUTIVE TYPE AIRCRAFT
  15. CHAPTER 5. FAN JET FALCON DESIGN AND CERTIFICATION TESTS
  16. CHAPTER 6. THE APPLICATION OF Ti-6A1-4V TITANIUM TO HELICOPTER FATIGUE LOADED COMPONENTS
  17. CHAPTER 7. THE FATIGUE AND FAIL-SAFE PROGRAM FOR THE CERTIFICATION OF THE LOCKHEED MODEL 286 RIGID ROTOR HELICOPTER
  18. CHAPTER 8. AGRICULTURAL AIRCRAFT FLIGHT LOADS: TYPICAL SPECTRA AND SOME OBSERVATIONS ON AIRWORTHINESS
  19. CHAPTER 9. THE NEW ZEALAND LIGHT AIRCRAFT FATIGUE METER PROGRAM
  20. CHAPTER 10. AN ASSESSMENT OF REPEATED LOADS ON GENERAL AVIATION AND TRANSPORT AIRCRAFT
  21. CHAPTER 11. EXTREME VALUE ANALYSIS OF FLIGHT LOAD MEASUREMENTS
  22. CHAPTER 12. UNDERCARRIAGE LOADINGS OF THREE AIRCRAFT: PORTER PC-6, VENOM DH-112 AND MIRAGE HIS
  23. CHAPTER 13. SOME CONSIDERATIONS ON ACOUSTIC FATIGUE
  24. CHAPTER 14. THE IMPORTANCE OF SERVICE IN SPECTIONIN AIRCRAFT FATIGUE
  25. CHAPTER 15. DESIGN PHILOSOPHY AND FATIGUE TESTING OF THE CONCORDE
  26. CHAPTER 16. FATIGUE DESIGN AND TEST PROGRAM FOR THE AMERICAN SST
  27. CHAPTER 17. ECONOMIC AND OPERATIONAL ASPECTS OF FATIGUE—FIGURES OF A SWISS GROUND ATTACK/FIGHTER AIRCRAFT
  28. CHAPTER 18. ECONOMIC ASPECTS OF FATIGUE IN COMMERCIAL AIRLINES
  29. CHAPTER 19. SOME THOUGHTS ON THE ECONOMICS OF FATIGUE
  30. CHAPTER 20. OBSERVATIONS ON DESIGNING TO COMBAT FATIGUE AND ITS EFFECTS ON THE ECONOMICS OF CIVIL TRANSPORT AIRCRAFT
  31. CHAPTER 21. DISCUSSION
  32. INDEX