Abstract
During a Lagrangian icing simulation a large number of droplet
trajectories are calculated to determine the water catch, and as a
result it is important that this procedure is as rapid as possible. In
order to arrive at a method with minimum complexity, a finite-volume
representation is developed for streamlines and extended to incorporate
the equations of motion for a droplet, with all cells being crossed in a
single timestep. However, since cells vary greatly in size, the method
must be implicit to avoid an awkward stability restriction that would
otherwise degrade performance. An implicit method is therefore
implemented by carrying out iterations to solve for the crossing of each
CFD cell, so that the droplet motion is tightly coupled to the
underlying flow and mesh. By crossing every cell in a single step, and
by using the mesh connectivity to track the droplet motion between
cells, any need for costly searches or containment checks is eliminated
and the resulting method is efficient. The implicit system is solved
using functional iteration, which is feasible for the droplet system
(which can be stiff) by using a particular factorisation. Stability of
this iteration is explored and seen to depend primarily on the maximum
power used in the empirical relationship for droplet drag coefficient CD = CD(Re),
while numerical tests confirm the theoretical orders of accuracy for
the different discretisations. Final results are validated against
experimental and alternative numerical water catch data for a NACA 23012
aerofoil.
| Original language | English |
|---|---|
| Pages (from-to) | 185-194 |
| Number of pages | 10 |
| Journal | International Journal of Multiphase Flow |
| Volume | 58 |
| DOIs | |
| Publication status | Published - Jan 2014 |
Bibliographical note
Date of Acceptance: 23/08/2013Keywords
- Particle tracking
- Icing
- CFD
- Droplet motion
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Dr Thomas C S Rendall
- School of Civil, Aerospace and Design Engineering - Associate Professor
- Fluid and Aerodynamics
Person: Academic , Member