Home Contact Sitemap

DTD Handbook

Handbook for Damage Tolerant Design

  • DTDHandbook
    • About
    • Contact
    • Contributors
    • PDF Versions
    • Related Links
    • Sections
      • 1. Introduction
      • 2. Fundamentals of Damage Tolerance
      • 3. Damage Size Characterizations
      • 4. Residual Strength
      • 5. Analysis Of Damage Growth
      • 6. Examples of Damage Tolerant Analyses
      • 7. Damage Tolerance Testing
      • 8. Force Management and Sustainment Engineering
        • 0. Force Management and Sustainment Engineering
        • 1. Force Structural Management
        • 2. Sustainment Engineering
        • 3. References
      • 9. Structural Repairs
      • 10. Guidelines for Damage Tolerance Design and Fracture Control Planning
      • 11. Summary of Stress Intensity Factor Information
    • Examples

Section 8.3. References

A.P. Berens, D.S. Morcock, K.E. Brown, J.C. Davis, R.L. Johnson, C.E. Larson, and D.J. White (1981, April).  “Handbook of Force Management Methods”.  AFWAL-TR-81-3079.  Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base, Ohio, 45433.

A.P. Berens, P.W. Hovey, and D.A. Skinn, (1991).  Risk Analysis for Aging Aircraft Fleets, Volume 1 – Analysis”.  WL-TR-91-3066, Wright Laboratory, Wright-Patterson Air Force Base, OH, 45433, 1991.

C. Brooks, K. Honeycutt, and S. Prost (2001).  “Monitoring the Robustness of Corrosion and Fatigue Prediction Models”.  Proceedings of the 2001 USAF Structural Integrity Program Conference, Williamsburg, Virginia.

L.E. Clay, N.H. Sandlin, D.S. Morcock, K.E. Brown, R.L. Johnson, and J.C. Davis (1978, December).  Force Management Methods Task I Report – Current Methods”.  AFFDL-TR-
78-183.  Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base, Ohio, 45433.

P.W. Hovey, A.P. Berens, and J.S. Loomis (1998).  “Update of the Probability of Fracture (PROF) Computer Program for Aging Aircraft Risk Analysis, Volume 1 Modifications and User’s Guide”.  AFRL-VA-WP-TR-1999-3030.  Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, 45469.

M. Lang, T. Hack, and V. Holzinger (2001).  “Technology for Corrosion Management of
Aging Aircraft”. 
Proceedings of the 2001 USAF Structural Integrity Program Conference, Williamsburg, Virginia.

J.W. Lincoln (2000).  “Aging Systems and Sustainment Technology”.  Structures Technology for Future Aerospace Systems, Volume 188, Progress in Astronautics and Aeronautics.  Ahmed K. Noor, (Ed.).

J.W. Lincoln (1997).  “Risks Assessments of Aging Aircraft”.  Proceedings of the First Joint DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah.

NTSB/AAR-89/03 (1989).  National Transportation Safety Board Aircraft Accident Report, Aloha Airlines, Flight 243, Boeing 737-200, N73711, near Maui, Hawaii, April 28, 1988.

D. Peeler, D. Raizenne, P. Sjoblom, J. Snide, and R. Rondeau (2001).  “Transitioning of the Retrogression and Re-Aging (RRA) Process to USAF Hardware”.  Proceedings of the 2001 USAF Structural Integrity Program Conference, Williamsburg, Virginia.

R. Selder and Liu Ko-Wei (1997).  “C-17A Individual Aircraft Tracking Program”.  Proceedings of the 1997 USAF Structural Integrity Program Conference, San Antonio, Texas.

T. Swift (1993).  “WFD Monitoring Issues and Concern”.  5th International Conference on Structural Airworthiness of New and Aging Aircraft, Hamburg, Germany.

T. Swift (1992b).  “Damage Tolerance Capability”.  Fatigue of Airacraft Metals.  Delft University Press, Proceedings of the Specialists’ Conference Dedicated to the 65th Birthday
 of J. Schijve
.  Delft, The Netherlands.

T. Swift (1992a).  “Unarrested Fast Fracture”.  Durability of Metal Aircraft Structures, Atlanta Technology Publications, Proceedings of the International Workshop on Structural Integrity of Aging Aircraft.

T. Swift (1987).  “Damage Tolerance in Pressurized Fuselages”.  14th Symposium of the International Committee on Aeronautical Fatigue, 11th Plantema Memorial Lecture, Ottawa, Canada, pp.1-77.