IC-117 Fatigue Loads as an Inverse Problem of the Helicopter Tail Beam Structural Dynamics
23rd:; Symposium, International Committee on Aeronautical Fatigue; ICAF 2005: structural integrity of advanced aircraft and life extension for current fleets: lessons learned in 50 years after the Comet accidents ; 2005 ; Hamburg, Germany
2005-01-01
10 pages
Conference paper
English
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FATIGUE LOADS AS AN INVERSE PROBLEM OF THE HELICOPTER TAIL BEAM STRUCTURAL DYNAMICS
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