Effect of phase change in a debris cloud on a backwall structure
- Sandia National Laboratories, Albuquerque, New Mexico 87185 (United States)
The physical state of a debris cloud generated upon impact of a thin flier plate with a thin bumper depends on the impact velocity. At impact velocities of 10 km/s, the debris cloud is expected to be primarily molten with some vapor present. A series of calculations using the finite-difference code CTH has been used to evaluate the effect of phase change (i.e., higher concentrations of vapor) in debris clouds and their subsequent impact on a backwall structure. In these calculations, the higher concentrations of vapor is achieved by increasing the initial temperature of the impactor and the bumper material while keeping the same impact velocity. The nature of the interaction of the debris cloud and the subsequent loading on the backwall depends on its thermophysical state. This interaction (with a backwall) can cause either spallation, rupture, or simply bulging of the backwall structure. These results will be discussed and compared with an impact experiment performed at [approx]10 km/s on the Sandia hypervelocity launcher. In the experiment, the debris cloud was generated by the impact of a titanium plate with a titanium bumper. [copyright]American Institute of Physics
- DOE Contract Number:
- AC04-76DP00789
- OSTI ID:
- 7019422
- Report Number(s):
- CONF-921145--
- Journal Information:
- AIP Conference Proceedings (American Institute of Physics); (United States), Journal Name: AIP Conference Proceedings (American Institute of Physics); (United States) Vol. 309:1; ISSN 0094-243X; ISSN APCPCS
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
360103* -- Metals & Alloys-- Mechanical Properties
CALCULATION METHODS
COMPUTERIZED SIMULATION
ELEMENTS
EVAPORATION
FINITE DIFFERENCE METHOD
FRAGMENTATION
IMPACT SHOCK
ITERATIVE METHODS
MELTING
METALS
NUMERICAL SOLUTION
PHASE TRANSFORMATIONS
SIMULATION
SPACE VEHICLES
TITANIUM
TRANSITION ELEMENTS
VEHICLES