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Elastic Instability (Buckling) of Sandwich Plates

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

Keywords

Sandwich Plate Sandwich Panel Unit Width Foam Core Honeycomb Core 
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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16.12 References

  1. 16.1.
    Anon (1955) Materials, Properties and Design Criteria Part II, Sandwich Construction for Aircraft, Military Handbook 23 (ANC-23), Department of the Air Force Research and Development Command; Department of the Navy, Bureau of Aeronautics; and Department of Commerce, Civil Aeronautics Administration, 2nd Edition.Google Scholar
  2. 16.2.
    Heath, W.G. (1960) Sandwich Construction, Part 2: The Optimum Design of Flat Sandwich Panels, Aircraft Engineering, Vol. 32, August, pp. 230–235.Google Scholar
  3. 16.3.
    Hemp, (1948) On a Theory of Sandwich Construction, College of Aeronautics Report, No. 15.Google Scholar
  4. 16.4.
    Hoff, N.J. and Mautner, S.E. (1945) Buckling of Sandwich Type Panels, Journal of the Aeronautical Sciences, Vol. 12, No. 3, pp. 285–297.CrossRefGoogle Scholar
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  7. 16.7.
    Libove, C. and Hubka, R.E. (1951) Elastic Constants for Corrugated-Core Sandwich Plates, NACA TN 2289.Google Scholar
  8. 16.8.
    Anderson, M.S. (1959) Optimum Proportions of Truss Core and Web-Core Sandwich Plates Loaded in Compression, NASA TN D-98, September.Google Scholar
  9. 16.9.
    Seide, P. (1952) The Stability Under Longitudinal Compression of Flat Symmetric Corrugated-Core Sandwich Plates with Simply Supported Loaded Edges and Simply Supported or Clamped Unloaded Edges, NACA TN 2679.Google Scholar
  10. 16.10.
    Kuenzi, E.W., Ericksen, W.S. and Zahan, J., Shear Stability of Flat Panels of Sandwich Construction, Forest Products Laboratory Report 1560, Rev. N62-13403.Google Scholar
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    Anderson, M.S. (1959) Local Instability of the Elements of a Truss-Core Sandwich Plate, NASA TR R-30.Google Scholar
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    Vinson, J.R. and Shore, S. (1967) Structural Optimization of Flat Corrugated Core Sandwich Panels Under In-Plane Shear Loads and Combined Uniaxial Compression and In-Plane Shear Loads, Naval Air Engineering Center Report NAEC-ASC-1110, July.Google Scholar
  13. 16.13.
    Vinson, J.R. (1986) Minimum Weight Triangulated (Truss) Core Composite Sandwich Panels Subjected to In-Plane Shear Loads, in Composites 86 — Recent Advances in Japan and the United States, Eds. K. Kawata, S. Umekawa and A. Kobayashi, Proceedings of the Third Japan-U.S. Conference on Composite Materials, Japan Society of Composite Materials, Publishers, Tokyo, pp. 663–671Google Scholar
  14. 16.14.
    Librescu, L., Hause, T. and Camarda, C.J. (1997) Geometrically Nonlinear Theory of Initially Imperfect Sandwich Curved Panels Incorporating Nonclassical Effects, AIAA Journal, Vol. 35, No. 8, August, pp. 1393–1403.CrossRefzbMATHGoogle Scholar
  15. 16.15.
    Smidt, S. (1996) Testing of Curved Sandwich Panels and Comparison with Calculations Based on the Finite Element Method, in Sandwich Construction 3 — Proceedings of the Third International Conference on Sandwich Construction, Southampton, Great Britain, Editor, H.G. Allen, EMAS Publications, United Kingdom, pp. 665–680.Google Scholar
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    Meunier, M. and Shenoi, R.A. (1999) Dynamic Behavior of Composite Sandwich Structures Modified Using HSOT, Proceedings of the European Conference on Computational Mechanics, Munich, September.Google Scholar
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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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