Damage assessment of nuclear containment against aircraft crash

Abstract The behavior of nuclear containment structure has been studied against aircraft crash with an emphasis on the influence of strike location. The impact locations identified on the BWR Mark III type nuclear containment structure are mid-height, junction of dome and cylinder, crown of dome and arc of dome. The containment at each of the above locations has been impacted normally by Phantom F-4, Boeing 707-320 and Airbus A320 aircrafts. The loading of the aircraft has been assigned through the corresponding reaction-time response curve. ABAQUS/Explicit finite element code has been used to carry out the three-dimensional numerical simulations. The concrete damaged plasticity model was used to simulate the behavior of concrete while the behavior of steel reinforcement was incorporated using the Johnson–Cook elasto-viscoplastic material model. The mid-height of containment has been found to experience most severe deformation against each aircraft. Phantom F4 has been found to be most disastrous at each location. The results have been compared with those of the available studies with respect to the containment deformation.

[1]  D. A. Godfrey,et al.  Structural analysis of aircraft impact on a nuclear containment vessel and associated structures , 1970 .

[2]  Martin Oliver,et al.  Comparison of different Constitutive Models for Concrete in ABAQUS/Explicit for Missile Impact Analyses , 2010 .

[3]  E. Oñate,et al.  A plastic-damage model for concrete , 1989 .

[4]  D. K. Paul,et al.  Aircraft crash upon outer containment of nuclear power plant , 1996 .

[5]  A. Siefert,et al.  Nonlinear analysis of commercial aircraft impact on a reactor building—Comparison between integral and decoupled crash simulation , 2014 .

[6]  M.N.Keshava Rao,et al.  Damage-zones of containment structures under aircraft impact loads , 1994 .

[7]  Jeeho Lee,et al.  Plastic-Damage Model for Cyclic Loading of Concrete Structures , 1998 .

[8]  Pradeep Bhargava,et al.  Numerical simulation of aircraft crash on nuclear containment structure , 2012 .

[9]  Pradeep Bhargava,et al.  Nuclear containment structure subjected to commercial and fighter aircraft crash , 2013 .

[10]  Th. Zimmermann,et al.  Dynamic rupture analysis of reinforced concrete shells , 1976 .

[11]  Jorge Daniel Riera,et al.  On the stress analysis of structures subjected to aircraft impact forces , 1968 .

[12]  Mukesh Kukreja Damage evaluation of 500 MWe Indian Pressurized Heavy Water Reactor nuclear containment for aircraft impact , 2005 .

[13]  Odd Sture Hopperstad,et al.  Perforation of 12 mm thick steel plates by 20 mm diameter projectiles with flat, hemispherical and conical noses: Part II: numerical simulations , 2002 .

[14]  T. Sugano,et al.  Full-Scale Aircraft Impact Test for Evaluation of Impact Forces, Part 1: Test Plan, Test Method, and Test Results , 1989 .

[15]  D. Agard,et al.  Microtubule nucleation by γ-tubulin complexes , 2011, Nature Reviews Molecular Cell Biology.

[16]  F. A. Leckie,et al.  Creep problems in structural members , 1969 .

[17]  Ernest Hinton,et al.  Numerical methods and software for dynamic analysis of plates and shells , 1988 .

[18]  D. K. Paul,et al.  Reaction-time response of aircraft crash , 1995 .

[19]  Giuseppe Forasassi,et al.  Preliminary evaluation of aircraft impact on a near term nuclear power plant , 2011 .

[20]  Jorge Daniel Riera A critical reappraisal of nuclear power plant safety against accidental aircraft impact , 1980 .

[21]  G. R. Johnson,et al.  Fracture characteristics of three metals subjected to various strains, strain rates, temperatures and pressures , 1985 .