FATIGUE, FRACTURE MECHANICS & DAMAGE TOLERANCE

COURSE OUTLINE

  1. 150 YEARS OF FATIGUE MISHAPS & Counting! 1 hour
    Structural Failure Modes: Creep, Fatigue, Corrosion, Wear, Fretting. Why "High-Strength" Materials Are weak In Fatigue
  2. CRACK INITIATION AND PROPAGATION: DESIGN STRATEGIES TO COMBAT FATIGUE 2 hours
    What is a FAILURE? USAF-Navy-FAA-NASA Guidelines, Case Study: Cracking In F-16 Fighters: US Navy & USAF Safety Factor Fantasies -- The Chippewa Effect, Infant Mortality. F-111 Crash: Dawn of FAIL-SAFE Policy Crack Arrest and Multiple Load Paths Case Study: Sioux City 1989 DC-10 Crash
  3. FRACTOGRAPHY 1 hour
    Beach Marks, Striations, Demo of Parts Failed by Fatigue
  4. CRACK INITIATION PROBLEMS 2 hours
    S-N CURVES, Endurance Limit and Fatigue Strength Surface & Size effects, STRESS CONCENTRATION Data, Load Streamlines Analogy, Classroom Exercises in Crack Initiation
  5. MEAN STRESS EFFECTS 1 hour
    GOODMAN & HAIGH Diagrams, Design Charts, Problems
  6. LOW-CYCLE FATIGUE 2 hours
    Neuber Notch Strain Analysis, Example Problems Data For Aerospace Materials
  7. MINER'S MYTH 1 hour
    Limited Applicability of Cumulative Damage, Dangers in Over-Reliance, Other Methods, Sample Data
  8. FRACTURE MECHANICS 5 hours
    DA Vinci & Griffith Experiments
    The Stress Intensity Factor
    Fracture Toughness -- Thickness & Directionality Effects
    Residual Strength Paris, Forman, & Walker Equations
    Example Crack Growth Calculations
    The Principle of Superposition, Compounding, Beta Factors
    Exercises using Stress Intensity Factor Handbook
    The Surface Crack
    Cracked Lugs, Stiffeners
    Variable Amplitude Loading; Retardation
    Willenborg, Wheeler, and Closure Models
    Dynamic Fracture; Adhesives
    Multiaxial Loadings -- Mixed Mode Crack Problems
  9. CRACKING AT STRUCTURAL HOLES 2 hours
    Loaded Holes Solution Methods
    Stop-Drill Technical Data
    Demo: StopCrack, ForceMate, & Coldworking of Holes
  10. DAMAGE TOLERANCE 2 hours
    Slow Crack Growth Structure
    Multiple Load Path Structure
    Continuing Damage & Multi-Site Damage
    FAA FAR 25.571 and 1529
    USAF MIL-A-83444 & MIL-A-87221A
    Demo: Fatigue-Fuse & Krak-Gage
    ASIP - Aircraft Structural Integrity Pgm.
    Individual Aircraft Tracking -- IATP
  11. COMPOSITES 2 hours
  12. BEARINGS, SHAFTS, SPRINGS, RIVETS 1 hour
  13. NDE 1 hour
    Important Inspection Methods -- Applicability, Reliability, Probability of Detection, Ultra Imaging, MagRubber, Eddy Scan
  14. PRESSURE VESSELS 1 hour
    ASME Boiler Code, Leak Before Break, Cases: Comet, Aloha Convertible-in-the-sky!
  15. LOAD SPECTRUM DEVELOPMENT 1 hour
    Sequence Effects, Truncation, Clipping, Retardation
  16. CRACK GROWTH COMPUTER PROGRAMS 1 hour
    CRACKS, ENDURE, FLAGRO, MODGRO, LUGGRO, FATLIF
  17. AGING AIRCRAFT ISSUES 1 hour
    FAA, Airlines, Navy, USAF Guidelines, Retrofits
  18. SHORT CRACKS 1 hour
  19. CORROSION FATIGUE 2 hours
    Case Study: A Landing Gear Failure
  20. FRETTING FATIGUE 1 hour
    Case Study: A Helicopter Lug Failure
  21. STRESS CORROSION CRACKING 2 hours
    Case Study: SCC of an Improperly Repaired Aircraft Structure
  22. WELDS-BREEDING GROUND FOR CRACKS 2 hours
    Porosity, Residual Stress, Reinforcement, Beta Factors,
    Hot Cracking, S-N & da/dN Data
  23. HELPFUL TREATMENTS & PROCESSES 1 hour
    Examples of Bad Design & Improvements, Residual Stress, Demo: Rollscan, Stresscan, Barkhausen Noise, SHOT-PEENING Advantages & Limitations, SHOT PEENING Manual
  24. CRACKED PARTS REPAIR PROCEDURES 1 hour
    Videos On Boron/Epoxy Repair, Case Study -- Boeing 747 Japan Airlines Crash, 1985
  25. FATIGUE, CRACK GROWTH & DTA TESTS 1 hour
    Specimen, Coupon, Component, & Full-Scale Tests
    ASTM Test Methods E399 & E647, Test Machines
  26. OPTIONALS (enter # in your Registration Form)
    1. Bearings --- Pitting & Spalling Fatigue
    2. Sonic Fatigue
    3. Creep & Thermal Fatigue, Radiation
    4. Weibull Parameters for Reliability
    5. Fatigue in Helicopters
    6. Fatigue of Polymers
"The strong point in the course was that we practiced how to apply fatigue concepts in dealing with practical applications." ----------------------------------------------------------------------
Tel: +1 (916) 933-3360 1 (800) 34-CRACK

FATIGUE CONCEPTS

FAX: +1 (916) 933-3361 1 (800) 342-7225
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Last updated: G3E (14 Mar 1996)