Investigation on impact resistance of steel plate reinforced concrete barriers against aircraft impact. Pt.2: Simulation analysis of scale model impact tests
- 1. Kobori Research Complex Inc., Kazuyoshi Kobayashi (Japan)
- 2. The Tokyo Electric Power Company (Japan)
Description
Steel plate reinforced concrete (SC) structure is one in which the rebars of conventional reinforced concrete (RC) structures are replaced with external steel plates attached to inner concrete with headed studs. SC structures are considered to be more effective than RC structures against aircraft impact, so their application to outer walls and roofs of risk-sensitive structures such as nuclear-related structures is expected to mitigate damage to critical components. The objective of this study was to investigate the fracture behavior and perforation thickness of SC panels against aircraft impact through impact tests and simulation analyses. Objectives of this paper are to analytically investigate the protection performance of SC panels against aircraft model impact through simulation analyses of 1/7.5 scale aircraft model impact tests presented in Part 1 of this study using a discrete element method (DEM), and to examine the applicability and validity of the DEM. Simulation analyses by a finite element method (FEM) were also performed to evaluate its applicability. The fracture process and damage to the SC test panels as well as the aircraft models are closely simulated by the discrete element analyses. The various impact responses and failure mechanisms, such as deceleration curves of projectile, velocity of debris from rear face and deformation mode of SC panels, are also simulated closely by the DEM analyses. The results of analyses confirm the shock-proof performance of SC panels against aircraft impact, and the applicability and validity of DEM for evaluating the complex phenomena of an aircraft impact against an SC panel. The finite element analysis closely simulates the deformation of the SC test panel and strains of rear steel plate where the global bending deformation mode is dominant. (authors)
Additional details
Publishing Information
- Publisher
- Atomic Energy Press
- Imprint Place
- Beijing (China)
- ISBN
- 7-5022-3421-7
- Imprint Title
- Proceedings of 18th international conference on structural mechanics in reactor technology
- Imprint Pagination
- 4896 p.
- Journal Page Range
- p. 2580-2590
Conference
- Title
- 18. international conference on structural mechanics in reactor technology
- Dates
- 7-12 Aug 2005
- Place
- Beijing (China)
INIS
- Country of Publication
- China
- Country of Input or Organization
- China
- INIS RN
- 43021564
- Subject category
- S42: ENGINEERING;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- AIRCRAFT; BENDING; COMPUTERIZED SIMULATION; CONTAINMENT BUILDINGS; DAMAGE; DEFORMATION; FINITE ELEMENT METHOD; FRACTURES; IMPACT TESTS; PERFORATION; PERFORMANCE; PLATES; REACTORS; REINFORCED CONCRETE; SCALE MODELS; STEELS; THICKNESS; VELOCITY; WALLS
- Descriptors DEC
- ALLOYS; BUILDING MATERIALS; BUILDINGS; CALCULATION METHODS; CARBON ADDITIONS; COMPOSITE MATERIALS; CONCRETES; CONTAINMENT; DEFORMATION; DIMENSIONS; FAILURES; IRON ALLOYS; IRON BASE ALLOYS; MATERIALS; MATERIALS TESTING; MATHEMATICAL SOLUTIONS; MECHANICAL TESTS; NUMERICAL SOLUTION; REINFORCED MATERIALS; SIMULATION; STRUCTURAL MODELS; TESTING; TRANSITION ELEMENT ALLOYS
Optional Information
- Notes
- 12 figs., 1 tab., 9 refs.