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Title

BALLISTIC LIMIT CALCULATION FOR ALUMINUM HONEYCOMB PANELS UNDER IMPACT OF RIGID CYLINDRICAL PROJECTILES

Pages

  790-801

Abstract

 In this paper IMPACT of rigid cylindrical projectiles on aluminum HONEYCOMB panels is studied. Considering various failure modes of target structure (including cell walls tearing and their folding and shearing of plug) by applying energy balance the BALLISTIC LIMIT velocity of panel is determined analytically. It is assumed that the HONEYCOMB behaviour is rigid, perfectly plastic and the projectile diameter is greater than the cell size. The results show that the BALLISTIC LIMIT velocity is increased by increasing the panel thickness, the compressive and shear strength of HONEYCOMB material and the walls thickness. However increasing the cell size, density, and the length of projectile the velocity decneases. The results of this analysis is in good agreement with experimental data.

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    APA: Copy

    LIAGHAT, GH.H., DAGHYANI, H.R., SADIGHI, M., & ALAVINIA, A.. (2003). BALLISTIC LIMIT CALCULATION FOR ALUMINUM HONEYCOMB PANELS UNDER IMPACT OF RIGID CYLINDRICAL PROJECTILES. AMIRKABIR, 14(55-B), 790-801. SID. https://sid.ir/paper/1014/en

    Vancouver: Copy

    LIAGHAT GH.H., DAGHYANI H.R., SADIGHI M., ALAVINIA A.. BALLISTIC LIMIT CALCULATION FOR ALUMINUM HONEYCOMB PANELS UNDER IMPACT OF RIGID CYLINDRICAL PROJECTILES. AMIRKABIR[Internet]. 2003;14(55-B):790-801. Available from: https://sid.ir/paper/1014/en

    IEEE: Copy

    GH.H. LIAGHAT, H.R. DAGHYANI, M. SADIGHI, and A. ALAVINIA, “BALLISTIC LIMIT CALCULATION FOR ALUMINUM HONEYCOMB PANELS UNDER IMPACT OF RIGID CYLINDRICAL PROJECTILES,” AMIRKABIR, vol. 14, no. 55-B, pp. 790–801, 2003, [Online]. Available: https://sid.ir/paper/1014/en

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