NASA NTRS · 20210017617
An Automated Refinement Process for Particle Trajectory Methods in GlennICE
Abstract
Computational methods for ice accretion can simulate the impact of water drops and ice crystals on an aircraft surface in a Lagrangian reference frame or in the Eulerian reference frame. In the Eulerian reference frame, particles are considered a continuous fluid while in the Lagrangian frame individual particle trajectories are calculated. Methods that use the Eulerian reference frame are typically easier to develop as established modules used for continuum mechanics can be leveraged. The Eulerian systems can also be faster since the user does not have to simulate millions of particles in order to achieve good results. It is imperative therefore that a Lagrangian method optimize the release points of trajectories such that accurate solutions can be obtained while minimizing as much as possible the number of trajectories computed. This paper will present a methodology for this refinement process and demonstrate its effectiveness on sample three dimensional test cases.
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William Wright, David Rigby, Eric Galloway, Christopher Porter. An Automated Refinement Process for Particle Trajectory Methods in GlennICE. https://ntrs.nasa.gov/citations/20210017617
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