A growth model for catastrophic cracking in an RAAF aircraft

Engineering Failure Analysis

Volumn 3, Issue 3, 1996, Pages 191-201

  Goldsmith, N T ^a   Clark, G ^a   Barter, S A ^a  

^a AERO AND MAR RESEARCH LABORATORY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CRACK PROPAGATION; CRACKS; FAILURE ANALYSIS; FATIGUE OF MATERIALS; FATIGUE TESTING; LOADING; MATHEMATICAL MODELS; MODELS; SURFACES;

AIRCRAFT LIFTING APPROACHES; LOWER WING SPAR; TENSILE TEARING;

WINGS;

EID: 0030232809     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/1350-6307(96)00014-3     Document Type: Article

References (9)

1. M. D. Coffin and C. F. Tiffany, J. Aircraft 13(2), 93-98 (1976).
2. Military Specification, MIL-A-83444, Airplane Damage Tolerance Requirements, USAF (1974).
3. Military Standard, MIL-STD-1530A(11), Airplane Structural Integrity Program, Airplane Requirements, USAF (1975).
4. N. T. Goldsmith and G. Clark, In Evaluation and Techniques in Fractography (edited by B. M. Strauss and S. K. Putatunda), pp. 52-68, STP 1085, American Society for Testing and Materials, Philadelphia, PA (1990).
5. G. Clark, S. Drury and G. S. Jost, 5th Australian Aeronautical Conference, Melbourne (1993).
6. G. Clark, S. A. Barter and N. T. Goldsmith, In Durability and Structural Reliability of Airframes (edited by A. Blom), pp. 281-304, EMAS, Warley (1993).
7. A. F. Grandt Jr, T. D. Scheumann, R. E. Todd and A. J. Hinkle, Fatigue and Fracture of Engineering Materials and Structures, Vol. 16, No. 2, pp. 199-213 (1993).
8. G. G. Trantina and M. Barishpolsky, Engng Fracture Mech. 20, 1-10 (1984).
9. G. Clark, Int. J. Fracture 15, R179-181 (1979).