NASA NTRS ยท 19730057432
Reflection of a shock wave from a thermally accommodating wall - Molecular simulation.
Abstract
Reflection of a plane shock wave from a wall has been simulated on a microscopic scale using a direct simulation Monte Carlo technique of the type developed by Bird. A monatomic gas model representing argon was used to describe the fluid medium and a simple one-parameter accommodation coefficient model was used to describe the gas-surface interaction. The influence of surface accommodation was studied parametrically by varying the accommodation coefficient from zero to one. Results are presented showing the temporal variations of flow field density, and mass, momentum, and energy fluxes to the wall during the shock wave reflection process. The energy flux was used to determine the wall temperature history. Comparisons with experiment are found to be satisfactory where data are available.
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Deiwert, G. S.. 1973-08-01. Reflection of a shock wave from a thermally accommodating wall - Molecular simulation.. https://ntrs.nasa.gov/citations/19730057432
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