Failure of Hexagonal and Triangular Honeycomb Core Sandwich Panels
| Autor: | Rakesh K. Kapania, Udit Shah |
|---|---|
| Rok vydání: | 2020 |
| Předmět: |
020301 aerospace & aeronautics
Materials science Spacecraft business.industry Aerospace Engineering 02 engineering and technology 01 natural sciences Finite element method 010305 fluids & plasmas Shear modulus Honeycomb structure 0203 mechanical engineering 0103 physical sciences Ultimate tensile strength Honeycomb Composite material business Aerospace Sandwich-structured composite |
| Zdroj: | AIAA Journal. 58:4923-4940 |
| ISSN: | 1533-385X 0001-1452 |
| DOI: | 10.2514/1.j059461 |
| Popis: | Honeycomb sandwich panels are used in aerospace structures for their high stiffness-to-mass ratio. Reducing structural mass is critical in aircraft and spacecraft development due to its direct impa... |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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