Publications

Farfan, Bernardo G.; Thornhill, Tom F.; Alexander, Charles S.; Reinhart, William D.

Abstract not provided.

Farfan, Bernardo G.; Thornhill, Tom F.; Alexander, Charles S.; Reinhart, William D.

Abstract not provided.

Journal of Applied Physics

Seagle, Christopher T.; Reinhart, William D.; Lopez, A.; Hickman, Randy J.; Thornhill, Tom F.

The capability for statically pre-compressing fluid targets for Hugoniot measurements utilizing gas gun driven flyer plates has been developed. Pre-compression expands the capability for initial condition control, allowing access to thermodynamic states off the principal Hugoniot. Absolute Hugoniot measurements with an uncertainty less than 3% on density and pressure were obtained on statically pre-compressed fluid helium utilizing a two stage light gas gun. Helium is highly compressible; the locus of shock states resulting from dynamic loading of an initially compressed sample at room temperature is significantly denser than the cryogenic fluid Hugoniot even for relatively modest (0.27-0.38 GPa) initial pressures. The dynamic response of pre-compressed helium in the initial density range of 0.21-0.25 g/cm3 at ambient temperature may be described by a linear shock velocity (us) and particle velocity (up) relationship: us = C0 + sup, with C0 = 1.44 ± 0.14 km/s and s = 1.344 ± 0.025.

Vogler, Tracy V.; Root, Seth R.; Knudson, Marcus D.; Reinhart, William D.; Thornhill, Tom F.

Abstract not provided.

Lawrence, R.J.; Bessette, Gregory B.; Lawrence, R.J.; Chhabildas, Lalit C.; Reinhart, William D.; Thornhill, Tom F.; Saul, WVenner S.

The Eulerian hydrocode, CTH, has been used to study the interaction of hypervelocity flyer plates with thin targets at velocities from 6 to 11 km/s. These penetrating impacts produce debris clouds that are subsequently allowed to stagnate against downstream witness plates. Velocity histories from this latter plate are used to infer the evolution and propagation of the debris cloud. This analysis, which is a companion to a parallel experimental effort, examined both numerical and physics-based issues. We conclude that numerical resolution and convergence are important in ways we had not anticipated. The calculated release from the extreme states generated by the initial impact shows discrepancies with related experimental observations, and indicates that even for well-known materials (e.g., aluminum), high-temperature failure criteria are not well understood, and that non-equilibrium or rate-dependent equations of state may be influencing the results.

Vogler, Tracy V.; Thornhill, Tom F.; Chhabildas, Lalit C.; Vogler, Tracy V.

In the current study we are developing an experimental fracture material property test method specific to dynamic fragmentation. This test method allows the study of fracture fragmentation in a reproducible laboratory environment under well-controlled loading conditions. Motion and fragmentation of the specimen are diagnosed using framing camera, VISAR and soft recovery methods. Fragmentation properties of several steels, nitinol, tungsten alloy, copper, aluminum, and titanium have been obtained to date. The values for fragmentation toughness, and failure threshold will be reported, as well as effects in these values as the material strain-rate is varied through changes in wall thickness and impact conditions.

Chhabildas, Lalit C.; Chhabildas, Lalit C.; Reinhart, William D.; Thornhill, Tom F.; Bessette, Gregory B.; Saul, WVenner S.; Lawrence, R.J.; Kipp, Marlin E.

A systematic computational and experimental study is presented on impact generated debris resulting from record-high impact speeds recently achieved on the Sandia three-stage light-gas gun. In these experiments, a target plate of aluminum is impacted by a titanium-alloy flyer plate at speeds ranging from 6.5 to 11 km/s, producing pressures from 1 Mb to over 2.3 Mb, and temperatures as high as 15000 K (>1 eV). The aluminum plate is totally melted at stresses above 1.6 Mb. Upon release, the thermodynamic release isentropes will interact with the vapor dome. The amount of vapor generated in the debris cloud will depend on many factors such as the thickness of the aluminum plate, super-cooling, vaporization kinetics, the distance, and therefore time, over which the impact-generated debris is allowed to expand. To characterize the debris cloud, the velocity history produced by stagnation of the aluminum expansion products against a witness plate is measured using velocity interferometry. X-ray measurements of the debris cloud are also recorded prior to stagnation against an aluminum witness plate. Both radiographs and witness-plate velocity measurements suggest that the vaporization process is both time-dependent and heterogeneous when the material is released from shocked states around 230 GPa. Experiments suggest that the threshold for vaporization kinetics in aluminum should become significant when expanded from shocked states over 230 GPa. Numerical simulations are conducted to compare the measured x-ray radiographs of the debris cloud and the time-resolved experimental interferometer record with calculational results using the 3-D hydrodynamic wavecode, CTH. Results of these experiments and calculations are discussed in this paper.

Chhabildas, Lalit C.; Chhabildas, Lalit C.; Reinhart, William D.; Thornhill, Tom F.; Bessette, Gregory B.; Saul, WVenner S.; Lawrence, R.J.; Kipp, Marlin E.

Abstract not provided.

Chhabildas, Lalit C.; Reinhart, William D.; Kipp, Marlin E.; Thornhill, Tom F.; Grady, Dennis E.

Abstract not provided.

Thornhill, Tom F.; Reinhart, William D.; Chhabildas, Lalit C.; Chhabildas, Lalit C.

Abstract not provided.