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DTD Handbook

Handbook for Damage Tolerant Design

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    • Sections
      • 1. Introduction
        • 0. Introduction
        • 1. Historical Perspective on Structural Integrity in the USAF
        • 2. Overview of MIL-HDBK-1530 ASIP Guidance
        • 3. Summary of Damage Tolerance Design Guidelines
        • 4. Sustainment/Aging Aircraft
        • 5. References
      • 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
      • 9. Structural Repairs
      • 10. Guidelines for Damage Tolerance Design and Fracture Control Planning
      • 11. Summary of Stress Intensity Factor Information
    • Examples

Section 1.5. References

Air Force Regulation 80-13 (1976, July).  “Aircraft Structural Integrity Program”.

F.D. Boensch (1964, August).  “Fatigue Test Program, F-104G/MAP Aircraft”, Report No. FDL TDR 64-97, AFFDL, WPAFB, OH.

D.E. Brammer (1963, July).  “Structural Fatigue Test Program, F-105D Airplane”, Report No. ASD-TDR-63-505, AFFDL, WPAFB, OH.

N.J. Hoff (1955, January).  “From the Structural Standpoint”.  Journal of the Royal Aeronautical Society (Vol 59).

JSSG-2006 (1998, October).  “Joint Service Specification Guide, Aircraft Structures”.  Department of Defense.

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

H.B. Lowndes, Jr., et al. (1958, June).  “Detail Requirements of Structural Fatigue Certification Program”.  WCLS-TM-58-4.

MIL-A-83444 (1974, July).  “Military Specification – Airplane Damage Tolerance Requirements”, USAF.

MIL-A-87221 (1985, February).  “Military Specification – General Specifications for Aircraft Structures”, USAF.

MIL-HDBK-1530 (1996, November).  “Military Handbook – General Guidelines for Aircraft Structural Integrity Program”, USAF.

MIL-STD-1530 (1972, September).  “Military Standard – Aircraft Structural Integrity Program, Airplane Requirements”, USAF.

MIL-STD-1530A (1975, December). “Military Standard – Aircraft Structural Integrity Program, Airplane Requirements”, USAF.

G.R. Negaard (1980, June).  “The History of the Aircraft Structural Integrity Program”.  Report No. 680.1B, Aerospace Structures Information and Analysis Center, AFFDL/FBR, WPAFB, OH.

J.L. Rudd, T.M. Hsu, H.A. Wood (1979).  “Part-Through Crack Problems in Aircraft Structures”, Part-Through Crack Fatigue Life Prediction.  J.B. Chang (Ed.).  ASTM STP 687, American Society for Testing and Materials, pp.168-194.

D. Steadman, A. Carter, R. Ramakrishnan (1999, September).  “Characterization of MSD in an In-Service Fuselage Lap Joint”, Proceedings on CD of the Third Joint FAA/DoD/NASA Conference on Aging Aircraft, Albuquerque, New Mexico.

C. Tiffany, et al (1977).  “Aging of U.S. Air Force Aircraft – Final Report”, Committee on Aging of U.S. Air Force Aircraft, National Materials Advisory Board, Commission on Engineering and Technical Systems, National Research Council, NMAB-488-2, National Academy Press, Washington D. C.