SUITABILITY OF DIFFERENT CRACK GROWTH MODELS FOR ANALYSING MULTI-SITE DAMAGE IN AIRCRAFT STRUCTURAL CONFIGURATIONS
International congress; 26th, International Council of the Aeronautical Sciences; 8th AIAA Aviation Technology, Integration, and Operations (ATIO) ; 2008 ; Anchorage, Alaska
2008-01-01
30 pages
Held on CD-ROM. Also Known as ICAS 2008; Held in e-store (RMS)
Conference paper
English
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