Author/Authors :
Saberi Reza نويسنده NSTRI , Alinejad Majid نويسنده NSTRI , Mahdavi Mir Omid نويسنده Civil Engineering Faculty, K.N. Toosi University of Technology , Sepanloo Kamran نويسنده NSTRI
Abstract :
An aircraft crashing into a nuclear containment
may induce a series of disasters related to containment
capacity, including local penetration and perforation of the
containment, intensive vibrations, and fire ignited after jet
fuel leakage. In this study, structural safety of a reinforced
concrete containment vessel (RCCV) has been studied
against the direct hit of Airbus A320, Boeing 707-320 and
Phantom F4 aircrafts. ABAQUS/explicit finite element
code has been used to carry out the three-dimensional
numerical simulations. The impact locations identified on
the nuclear containment structure are mid height of containment,
center of the cylindrical portion, junction of
dome and cylinder, and over the cylindrical portion close to
the foundation level. The loading of the aircraft has been
assigned through the corresponding reaction-time response
curve. The concrete damaged plasticity model was predicted
to simulate the behavior of concrete while the
behavior of steel reinforcement was incorporated using
elastoplastic material model. Dynamic loading conditions
were considered using dynamic increase factor. The mid
height of containment and center of cylindrical portion
have been found to experience most severe deformation
against each aircraft crash. It has also been found that
compression damage in concrete is not critical at none of
the impact locations.