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NASA NTRS · 19880002489

Wake shield

Abstract

Progress on the modeling of the flow field around a wake shield using a recently obtained code based on the Monte Carlo method is discussed. The direct simulation Monte Carlo method is a method for solving the Boltzman Equation using an approximation to the collision integral term. The collision integrand is evaluated for randomly selected values of its arguments and the summation will approach the integral for large enough samples. The collision effects may be modeled for either hard sphere or various power law potentials. The convective side of the Boltzman equation is approximated over a time step using a simple trajectory calculation of molecules as they travel through the domain of interest.

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BibTeXRIS

Bannister, Tommy, Karr, Gerald R.. 1987-09-01. Wake shield. https://ntrs.nasa.gov/citations/19880002489

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