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Structural Optimization to Obtain Minimum Weight Sandwich Panels

  • Jack R. Vinson
Part of the Solid Mechanics and Its Applications book series (SMIA, volume 120)

Keywords

Sandwich Panel Foam Core Honeycomb Core Face Stress Optimum Construction 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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17.11 References

  1. 17.1.
    Vinson, J.R. (1985) Minimum Weight Composite Material Honeycomb Sandwich Panels Under Uniaxial Compression, Transactions of the First European Conference on Composite Materials, September.Google Scholar
  2. 17.2.
    Vinson, J.R. (1986) Optimum Design of Composite Honeycomb Sandwich Panels Subjected to Uniaxial Compression, AIAA Journal, Vol. 24, pp. 1690–1696.CrossRefzbMATHGoogle Scholar
  3. 17.3.
    Vinson, J.R. and Shore, S. (1967) Structural Optimization of Corrugated Core and Web Core Sandwich Panels Subjected to Uniaxial Compression, Naval Air Engineering Center Report NAEC-ASC-1109, May.Google Scholar
  4. 17.4.
    Vinson, J.R. (1986) Minimum Weight Web-Core Composite Sandwich Panels Subjected to In-Plane Compressive Loads, presented at the International Symposium on Composite Materials and Structures, Beijing, China, June 13–16.Google Scholar
  5. 17.5.
    Handel, P.I. and Vinson, J.R. (1988) Optimal Stacking Sequence of Composite Faces for Various Sandwich Panels and Loads to Attain Minimum Weight, Proceedings of the 29 th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, AIAA, pp. 999–1006.Google Scholar

Copyright information

© Springer 2005

Authors and Affiliations

  • Jack R. Vinson
    • 1
  1. 1.Center for Composite Materials and College of Marine Studies, Department of Mechanical Engineering, Spencer LaboratoryUniversity of DelawareNewarkUSA

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