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A numerical modeling for eigenvibration analysis of honeycomb sandwich panels

โœ Scribed by Tanimoto, Y.; Nishiwaki, T.; Shiomi, T.; Maekawa, Z.


Book ID
126626828
Publisher
Taylor and Francis Group
Year
2001
Tongue
English
Weight
279 KB
Volume
8
Category
Article
ISSN
0927-6440

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Experimental bird-strike tests have been carried out on double sandwich panels made from AlSi7Mg0.5 aluminium foam core and aluminium AA2024 T3 cover plates. The bird-strike velocity varied from 140 to 190 m/ s. The test specimens were instrumented with strain gauges in the impacted area to measure