Mathematical Modelling of Damage of Aircraft Skin Panels Subjected to Blast Loading

Authors

  • S.K. Singh Centre for Aeronautical System Studies and Analyses.
  • V.P. Singh Centre for Aeronautical System Studies and Analyses

DOI:

https://doi.org/10.14429/dsj.41.4434

Keywords:

Explosives, Aircraft safety, Mathematical model

Abstract

A mathematical model for assessing the damage to an aircraft due to blast from conventional ammunition has been developed. The minimum distance of the point of explosion from the aircraft for its permanent damage for a reference explosion has been obtained depending upon the dimensions (thin plate or thin cylindrical shell) of the structural elements.

Author Biographies

S.K. Singh, Centre for Aeronautical System Studies and Analyses.

Centre for Aeronautical System Studies and Analyses.

V.P. Singh, Centre for Aeronautical System Studies and Analyses

Centre for Aeronautical System Studies and Analyses

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Published

2013-01-01

How to Cite

Singh, S., & Singh, V. (2013). Mathematical Modelling of Damage of Aircraft Skin Panels Subjected to Blast Loading. Defence Science Journal, 41(3), 305–316. https://doi.org/10.14429/dsj.41.4434

Issue

Vol. 41 No. 3

Section

Aeronautical Systems

License

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