Abstract The failure energy of sandwich panels with cores of the M-crimp type is considered. The results of comparative tests for impact resistance of panels with folded cores of the M-crimp type and honeycomb cores are presented.
Analysis of folded structures for impact resistance
Russian Aeronautics (Iz VUZ) ; 50 , 4 ; 439-441
2007-12-01
3 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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