Damage tolerant risk analysis techniques for evaluating the structural integrity of aircraft structures

11th International Conference on Fracture 2005, ICF11

Volumn 1, Issue , 2005, Pages 71-76

  Gallagher, Joseph P ^a   Babish, Charles A ^a   Malas, James C ^b  

^a WRIGHT PATTERSON AIR FORCE BASE   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AGING AIRCRAFT; AIRCRAFT STRUCTURE; ANALYSIS TECHNIQUES; CRACKED STRUCTURES; DAMAGE TOLERANT; INSPECTION SCHEDULE; NONDESTRUCTIVE INSPECTION; RISK ASSESSMENT METHODOLOGIES; STRUCTURAL FAILURE; UNITED STATES AIR FORCE;

AIRCRAFT MANUFACTURE; AIRFRAMES; FRACTURE; FRACTURE MECHANICS; RISK ASSESSMENT; SAFETY ENGINEERING;

STRUCTURAL INTEGRITY;

EID: 84869821466     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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12. Berens, A.P., Hovey, P.W., and Loomis, J.S, " Update of the PROF Computer Program for Aging Aircraft Risk Analysis, Volume I - Modifications and User's Guide", Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, Nov 1998
13. Rummel, W.D. and Matzkanin, G.A., Nondestructive Evaluation Capabilities Data Book, NTIAC: DB-97-02, Nondestructive Testing Information Analysis Center (NTIAC), Austin, Texas, Nov 1997