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Wake shieldProgress 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.
Document ID
19880002489
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bannister, Tommy
(Wyle Labs., Inc. Huntsville, Ala., United States)
Karr, Gerald R.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Publication Information
Publication: Consortium for Materials Development in Space. Technical Section
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
88N11871
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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