A smeared stiffener model for vibration analysis of anisogrid-stiffened composite conical shells using differential quadrature method
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics
Link
https://link.springer.com/content/pdf/10.1007/s40430-023-04606-y.pdf
Reference46 articles.
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2. Vasiliev V, Razin A (2006) Anisogrid composite lattice structures for spacecraft and aircraft applications. Compos Struct 76(1–2):182–189. https://doi.org/10.1016/j.compstruct.2006.06.025
3. Vasiliev V, Razin A, Totaro G, De Nicola F (2005) Anisogrid conical adapters for commercial space application. AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.
4. Vasiliev VV, Barynin VA, Razin AF (2012) Anisogrid composite lattice structures–Development and aerospace applications. Compos Struct 94(3):1117–1127. https://doi.org/10.1016/j.compstruct.2011.10.023
5. Totaro G (2016) Flexural, torsional, and axial global stiffness properties of anisogrid lattice conical shells in composite material. Compos Struct 153:738–745. https://doi.org/10.1016/j.compstruct.2016.06.072
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