作者: H Fꎬ Wu , L Lꎬ Wu , WJ Slagter , JL Verolme , None
DOI: 10.1007/BF00376282
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摘要: This paper presents the results of a statistically designed programme conducted to validate feasibility using relationship mechanical properties and metal volume fraction in fibre-metal laminates make property predictions. Experimental analytical practices employed obtain these for tension, compression, in-plane shear, bearing are described. Results from this pilot study show that use may be useful prediction strength laminates. However, needs further concept. If hypothesis is valid, number laminate configurations tested qualify family can minimized. The findings imply approach rule mixtures exploited estimate design multitude variants, which economically beneficial preliminary stages aircraft design.