Tests made by de Havilland Aircraft Co; wing sustained repeated applications of different loadings between 1.5g and 4.37g, particular interest being focused on Redux joints between skin and stringers; fin sustained 60,000 cycles in reversal of 33% of fully factored load and 30 cycles in reversal of 66.7%.
Repeated loading and fatigue tests on D.H. 104 (Dove) wing and fin
Aircraft Eng
Aircraft Engineering ; 22 , n 256
1950
6 pages
Aufsatz (Zeitschrift)
Englisch
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Repeated Loading and Fatigue Tests on a D.H. 104 (Dove) Wing and Fin
Emerald Group Publishing | 1950
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