PROPOSED WORKING LIFE APPROACH FOR WELDED JOINTS : WITH APPLICATION TO AIRCRAFT STRUCTURES . | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 53, Volume 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, May 1985, Page 623-635 PDF (3.56 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.1985.26539 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| MOUSTAFA EL-GAMMAL1, 2, 3 | ||||
| 1Currently on Sabbatical leave from Faculty of Engineering, University of Alexandria, Alexandria, EGYPT.+ | ||||
| 2Winner of State Prize in Engineering Sciences, Egypt, 1903.+ | ||||
| 3Professor of Technology and Shibuilding Studies, THE ARAB GULF ACADEMY FOR MARITIME STUDIES, BASRAH, IRAQ. | ||||
| Abstract | ||||
| A proposed working life approach for welded joints in aircraft structures is investigated. This approach is based on the assumption that the crack propagation will be under clear monitored survey. The repairs, however, should be carried out at a level long before the welded joint may become in jeopardy.' Risk of failure and the cost effective of this risk are also included within the proposed approach. | ||||
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