Abstract
The Boltzmann equation is essential to the accurate modeling of rarefied gases. Unfortunately, traditional numerical solvers for this equation are too computationally expensive for many practical applications. With modern interest in hypersonic flight and plasma flows, to which the Boltzmann equation is relevant, there would be immediate value in an efficient simulation method. The collision integral component of the equation is the main contributor of the large complexity. A plethora of new mathematical and numerical approaches have been proposed in an effort to reduce the computational cost of solving the Boltzmann collision integral, yet it still remains prohibitively expensive for large problems. This paper aims to accelerate the computation of this integral via machine learning methods. In particular, we build a deep convolutional neural network to encode/decode the solution vector, and enforce conservation laws during post-processing of the collision integral before each time-step. Our preliminary results for the spatially homogeneous Boltzmann equation show a drastic reduction of computational cost. Specifically, our algorithm requires O(n3) operations, while asymptotically converging direct discretization algorithms require O(n6), where n is the number of discrete velocity points in one velocity dimension. Our method demonstrated a speed up of 270 times compared to these methods while still maintaining reasonable accuracy.
Highlights
While the Euler and Navier–Stokes equations have for a long time been the work horses in the modeling of fluid dynamics, these equations are inadequate for modeling complex flows, such as rarefied gases, for which the continuum assumption is invalid
A plethora of new mathematical and numerical approaches have been proposed in an effort to reduce the computational cost of solving the Boltzmann collision integral
Our preliminary results for the spatially homogeneous Boltzmann equation show a drastic reduction of computational cost, in the order of O(n3 ), compared to O(n6 ) for direct discretization algorithm of [6]
Summary
Rarefied gas flows have become a topic of increasing interest due to their relevance in practical applications such as hypersonic and space vehicles. As the governing equation of kinetic theory, the Boltzmann equation is key in understanding these interactions, and critical in aiding the successful design of these flight vehicles, as well as other applications. Despite the rapid increase in computing power of recent years, numerical solution of this equation continues to present a major challenge. Among the components of the equation, the main driver of computational complexity is the multi-dimensional collision integral. A plethora of new mathematical and numerical approaches have been proposed in an effort to reduce the computational cost of solving the Boltzmann collision integral
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