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Fatigue study on the cracks of a cannon

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Purpose: Cannon is one of the most usage parts in military industries and analysis of its pipe is very important. Therefore, the prediction of its longevity to say, the number of cannon ball that can be fired till it is break down should be under consideration. Design/methodology/approach: Since the life of cannon's barrel directly depends on the inner micro-cracks under numerous firing, the study of these cracks are very important. From this point of view, the stress analysis on crack tip is carried out via ANSYS software in this research. Findings: This analysis shows that the stress intensity on the tip of the crack is a function of its length and increases with the number of these cracks. Research limitations/implications: In this research the fatigue with several cracks is analyzed in the barrel according to the explosion pressure in order to find the critical conditions. Originality/value: Since the cannon barrel life is a convert function of the stress intensity of the cracks, multi-cracks condition passes the most fatigue cycling. The shape function of the cracks is also decreased with the number of the cracks.
Rocznik
Strony
59--62
Opis fizyczny
Bibliogr. 15 poz., tab., wykr.
Twórcy
  • School of Mechanical Engineering, Faculty of Engineering, University of Tehran, Tehran, Iran, mahdavin@ut.ac.ir
Bibliografia
  • [1] D. K. Wiatkowski, Determination of crack resistance on the basis of the J integral for talc filled PP and PA composites, Proceeding of the 13th International Scientific Conference on Achievements in Mechanical and Materials Engineering, AMME'2005, Gliwice-Wisła, 2005, 391-394.
  • [2] Y. Xiangqiao, A special crack-tip displacement discontinuity element, Journal of Mechanic Research Communications 31 (2004) 651-659.
  • [3] J. Wang, X. Zhou, Near crack line elastic-plastic analysis for a infinite plate loaded by two pairs of point tensile forces, Journal of Mechanic Research Communications 31 (2004) 415-420.
  • [4] S. Z. Qamar, T. Pervez, R. A. Siddiqui, A. K. Sheikh, A. F. M. Arif, Sensivity analysis in life prediction of extrusion die, Journal of Achievements in Materials and Manufacturing Engineering 25/1 (2007) 49-54.
  • [5] Z. G. Zhou, B. Wang, Y. G. Sun, Relationship of crack fabric tensors of different order, Proceedings of 7thWSEAS International Conference on Simulation, Modelling and Optimization, Beiging, China, 2007, 210-218.
  • [6] T. Ozben, A. Yardimeden, O. Cakir, Stress analysis of shrink-fitted pin-pin hole connections via Finite Element Method, Journal of Achievements in Materials and Manufacturing Engineering 25/1 (2007) 45-48.
  • [7] Q. Yang, X. Chen, L. G. Than, Investigation of the behaviour of a Griffith crack at the interface of a layer bonded to a half plane using the Schmidt method for opening crack mode, International Journal of Production Research 41 (2003) 4505-4517.
  • [8] J. R. Jain, T. K. Kundra, Model based online diagnosis of unbalance and traverse fatigue crack in rotor systems, Journal of Mechanism and Machine Theory 39 (2004) 1307-1315.
  • [9] M. Czechowski, Fatigue life of friction stir welded Al-Mg alloys, Proceeding of the 13th International Scientific Conference on Achievements in Mechanical and Materials Engineering AMME'2005, Gliwice-Wisła, 2005, 83-86.
  • [10] G. M. Jouris, J. M. Bloom, J. C. Ekvall, Probabilistic fracture mechanics and fatigue methods: applications for structural design and maintenance, American Society for Testing Materials 7 (1983) 141-176.
  • [11] M. Staszewski, Z. M. Rdzawski, A. Wrona, Residual stresses in the strips from copper-based alloys, Journal of Achievements in Materials and Manufacturing Engineering 25/2 (2007) 35-38.
  • [12] S. B. Leslie, R. Eliasi, Fatigue life analysis of a cannon barrel, Engineering Failure Analysis 6 (1999) 371-385.
  • [13] L. B. Sills, P. A. Wawrzynek, B. Carter, A. R. Ingraffea, I. Hershkovitz, Methods for calculating stress intensity factors in anisotropic materials: part II-arbitrary geometry, Engineering Fracture Mechanics 74 (2007) 1293-1307.
  • [14] L. B. Sills, V. Boniface, R. Eliasi, Development of a methodology for determination of interface fracture toughness of laminate composites-the 0o/90o pair, International Journal of Solids and Structures 42 (2005) 663-680.
  • [15] V. A. Avakov, Fatigue Reliability Functions in Semilogarhmic Coordinates: Reliability, Stress Analysis and Failure Prevention, ASME, 1991, 55-60.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BWAN-0002-0070
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