[1] Rohwer K., Friedrichs S., Wehmeyer C., Analyzing laminated structures from fiber-reinforced composite material-an assessment, Technische Mechanik, Vol. 25, No. 1, pp. 59-79, 2005.
[2] Silverman E., Rhodes M., Dyer M., Composite Isogrid Structures for Spacecraft Components, Society for the Advancement of Materials and Process Engineering Journal, Vol. 35, No. 1, pp. 51-58, 1999.
[3] Aktay L., Johnson A. F., Holzapfel M., Prediction of impact damage on sandwich composite panels, Computational Materials Science, Vol. 32, No. 3-4, pp. 252-260, 2005.
[4] Aktay L., Johnson A. F., Kroplin B. H., Numerical modeling of honeycomb core crush behavior, Engineering Fracture Mechanics, Vol. 75, No. 9, pp. 2616-2630, 2008.
[5] Foo C. C., Chai G. B., Seah L. K., A model to predict low-velocity impact response and damage in sandwich composites, Composites Science and Technology, Vol. 68, No. 6, pp. 1348-1356, 2008.
[6] Standard, Military standard sandwich constructions and core materials, general test methods, MIL-STD-401B, (USA): Department of Defense, 1967.
[7] Zhou G., Hill M., Loughlan J., Hookham N., Damage characteristics of composite honeycomb sandwich panels in bending under quasi-static loading. Journal of Sandwich Structures and Materials, Vol. 8, No. 1, pp. 55-90, 2006.
[8] Kreja I., Critical examination of benchmark problems for large rotation analysis of laminated shells, Shell Structures: Theory and Applications, Proceedings of The 8th Conf. SSTA, Gdansk-Jurata, Taylor & Francis Group, London, October, 12-14, 2005.
[9] Wahl L., Maas S., Waldmann D., Zurbes A., Freres P., Shear stresses in honeycomb sandwich plates: Analytical solution, finite element method and experimental verification, Journal of Sandwich Structures and Materials, Vol. 14, No.4, pp. 449-468. 2012.
[10] Peery D. J.,. Azar J. J, Aircraft Structures, New York: McGraw-Hill, 1982.
[11] H. D. Curtis, Fundamentals of Aircraft Structural Analysis, Chicago: Irwin, 1997.
[12] Bitzer T., Honeycomb Technology-Material Design, Manufacturing Applications and Testing, pp. 10-42, London: Springer Netherlands, 1997.
[13] Mohr D., Doyoyo M., Deformation-induced folding systems in thin walled monolithic hexagonal metallic honeycomb, International Journal of Solids and Structures, Vol. 41, No. 11, pp. 3353-3377, 2004.
[14] Hou B., Pattofatto S., Li Y. L., Zhao H., Impact behavior of honeycombs under combined shear-compression, Part II: Analysis, International Journal of Solids and Structures, Vol. 48, No. 5, pp. 698-705, 2011.
[15] Alavi Nia A., Razavi S., Majzoobi G., Ballistic limit determination of aluminum honeycombs-experimental study, Materials Science and Engineering, Vol. 448, No. 1, pp. 273-280, 2008.
[16] Liaghat GH., Alavi Nia A., Daghyani H. R., Sadighi M., Ballistic limit evaluation for impact of cylindrical projectiles on honeycomb panels, Thin-Walled Structures, Vol. 48, No. 1, pp. 55-61, 2010.