TECHNICAL PAPERS
Jul 1, 2006

Determination of Honeycomb Material Properties: Existing Theories and an Alternative Dynamic Approach

Publication: Journal of Aerospace Engineering
Volume 19, Issue 3

Abstract

This paper examines several available analytic and experimental methods to determine the orthotropic material properties of honeycomb. Fifteen published sets of simple equations for the material properties were reviewed and their values calculated for a specific honeycomb aluminum core. The same core was tested with ASTM standard methods and the agreement between the theoretical material properties and the experimental results was considered. To reduce the time and cost for the experimental determination, a simple technique for measuring the main dynamic material properties of honeycomb is introduced. A good agreement was found between the major theoretical out-of-plane material properties of honeycomb, the experimental ASTM methods, and the presented dynamic approach.

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References

Adams, R., and Maheri, M. (1993). “The dynamic shear properties of structural honeycomb materials.” Compos. Sci. Technol., 47(1), 15–23.
Albracht, F., Altenbach, H., and Nast, E. (1996). “On the prediction of effective elastic moduli of honeycomb-type sandwich plates.” Computer aided design in composite material technology, W. R. Blain and W. P. De Wilde, eds., Computational Mechanics, Southampton, U.K., 81–90.
ASTM. (1970). “C273 standard method of shear test in flatwise plane of flat sandwich constructions or sandwich cores.” ASTM C273, West Conshohocken, Pa.
ASTM. (1988a). “C271 standard test method for density of core materials for structural sandwich constructions.” ASTM C271, West Conshohocken, Pa.
ASTM. (1988b). “C365 standard test methods for flatwise compressive strength of sandwich cores.” ASTM C365, West Conshohocken, Pa.
ASTM. (2002). “D6790 standard test method for determining Poisson’s ratio of honeycomb cores.” ASTM D6790, West Conshohocken, Pa.
Bitzer, T. (1994). “Useful analysis methods for sandwich structures.” Proc., 39th Int. SAMPE Symp., SAMPE, Anaheim, Calif., 419–425.
Burton, W., and Noor, A. (1997). “Assessment of continuum models for sandwich panel honeycomb cores.” Comput. Methods Appl. Mech. Eng., 145(3–4), 341–360.
Chamis, C., Aiello, R., and Murthy, P. (1988). “Fibre composite sandwich thermostructural behavior: Computational simulation.” J. Compos. Technol. Res., 10(3), 93–199.
Feichtinger, K. (1989). “Test methods and performance of structural core materials. I: Static properties.” J. Reinf. Plast. Compos., 8, 334–357.
Gibson, L., and Ashby, M. (1988). Cellular solids: Structure and properties, Pergamon, Oxford, U.K.
Grediac, M. (1993). “A finite-element study of the transverse shear in honeycomb cores.” Int. J. Solids Struct., 30(13), 1777–1788.
Guo, X., and Gibson, L. (1999). “Behavior of intact and damaged honeycombs: A finite-element study.” Int. J. Mech. Sci., 41(1), 85–105.
Hexcel Composites. (2001). “Hexweb 3003 commercial grade aluminium honeycomb product data.” ⟨www.hexcelcomposites.com⟩ (Jan. 26, 2005).
Hoffman, G. (1958). “Poisson’s ratio for honeycomb sandwich cores.” J. Aerosp. Sci., 25(8), 534–535.
Hohe, J., and Becker, W. (2002). “Effective stress-strain relations for two-dimensional cellular sandwich cores: Homogenization, material models, and properties.” Appl. Mech. Rev., 55(1), 61–87.
Kelsey, S., Gellatly, R., and Clark, B. (1958). “The shear modulus of foil honeycomb cores.” Aircr. Eng., 30, 294–302.
Klintworth, J., and Stronge, W. (1988). “Elasto-plastic yield limits and deformation laws for transversely crushed honeycombs.” Int. J. Mech. Sci., 30(3–4), 273–292.
Meraghni, F., Desrumaux, F., and Benzeggagh, M. (1999). “Mechanical behavior of cellular core for structural sandwich panels.” Composites, Part A, 30(6), 767–779.
Mistou, S., Sabarots, M., and Karama, M. (2000). “Experimental and numerical simulations of the static and dynamic behavior of sandwich plates.” Proc., European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS, Barcelona, Spain.
Noor, A., Burton, W., and Bert, C. (1996). “Computational models for sandwich panels and shells.” Appl. Mech. Rev., 49(3), 155–199.
Norris, C. (1947). “An analysis of the compressive strength of honeycomb cores for sandwich constructions.” Technical Rep. No. NACA TN-1251, National Advisory Committee for Aeronautics.
Penzien, J., and Diriksson, T. (1964). “Effective shear modulus of honeycomb cellular structure.” AIAA J., 2(3), 531–35.
Ringelstetter, L., Voss, A., and Norris, C. (1950). “Effect of cell shape on compressive strength of hexagonal honeycomb structures.” Technical Rep. No. NACA TN-2243, National Advisory Committee for Aeronautics.
Shi, G., and Tong, P. (1995). “Equivalent transverse shear stiffness of honeycomb cores.” Int. J. Solids Struct., 32(10), 1383–1393.
Smallen, H., and Roberts, W. (1961). “Properties of stainless steel sandwich using low-density honeycomb cores.” Weld. J. (Miami, FL, U.S.), 40(2), 90s–96s.
Society of Automotive Engineers (SAE). (1999). “AMSSTD401 sandwich constructions and core materials: General test methods.” AMSSTD401.
Vinson, J. (1986). “Optimum design of composite honeycomb sandwich panels subjected to uniaxial compression.” AIAA J., 24(10), 1690–1696.
Werren, F., and Norris, C. (1950). “Analysis of shear strength of honeycomb cores for sandwich constructions.” Technical Rep. No. NACA TN-2208, National Advisory Committee for Aeronautics.
Zenkert, D. (1997). An introduction to sandwich construction, reprint, EMAS, London.
Zhang, J., and Ashby, M. (1992). “The out-of-plane properties of honeycombs.” Int. J. Mech. Sci., 34(6), 475–489.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 19Issue 3July 2006
Pages: 177 - 183

History

Received: Feb 15, 2005
Accepted: Jul 6, 2005
Published online: Jul 1, 2006
Published in print: Jul 2006

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Authors

Affiliations

C. W. Schwingshackl [email protected]
Graduate Student, Astronautics Research Group, School of Engineering Sciences, Univ. of Southampton, Highfield, Southampton SO17 1BJ, U.K. (corresponding author). E-mail: [email protected]
G. S. Aglietti
Senior Lecturer in Aerospace Structural Dynamics, School of Engineering Sciences, Univ. of Southampton, Highfield, Southampton SO17 1BJ, U.K.
P. R. Cunningham
Principal Stress Engineer, Composites, Smith Aerospace Mechanical Systems-Aerostructures, Kings Av., Hamble-le-Rice, Southampton SO31 4NF, U.K.

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