Results of numerical modeling of solid fuel melting and shedding by hot gas flow are presented. The computational model is based on the Volume-of-Fluid approach, implemented on a two-dimensional Cartesian grid, with one-equation turbulence model. Simulations are presented for a slab of wax interacting with a parallel gas flow, with the properties taken to be typical of hybrid engines (nitrous oxide). Development of Kelvin-Helmholtz instability in the melt layer is demonstrated, including the wave formation and droplet shedding by the flow.

1.
A.
Mazzetti
,
L.
Merotto
, and
G.
Pinarello
, “
Paraffin-based hybrid rocket engines applications: A review and a market perspective
,”
Acta Astronautica
126
,
286
(
2016
).
2.
A.
Karabeyoglu
,
G.
Zilliac
,
B. J.
Cantwell
,
S.
DeZilwa
, and
P.
Castellucci
, “
Scale-up tests of high regression rate paraffin-based hybrid rocket fuels
,”
Journal of Propulsion and Power
20
,
1037
(
2004
).
3.
A.
Weinstein
and
A.
Gany
, “
Testing and modeling liquefying fuel combustion in hybrid propulsion
,”
Progress in Propusion Physics
4
,
99
112
(
2013
).
4.
S.
Rashkovskiy
and
S.
Yakush
, “
Numerical simulation of low-melting temperature solid fuel regression in hybrid rocket engines
,”
Acta Astronautica
176
,
710
716
(
2020
).
5.
S. R.
Allmaras
,
F. T.
Johnson
, and
P. R.
Spalart
, “
Modifications and clarifications for the implementation of the Spalart-Allmaras turbulence model
,” in
Seventh International Conference on Computational Fluid Dynamics, ICCFD7-1902
(
2012
) pp.
1
11
.
6.
J. R.
Edwards
and
S.
Chandra
, “
Comparison of eddy viscosity-transport turbulence models for three-dimensional, shock-separated flowfields
,”
AIAA Journal
34
,
756
763
(
1996
).
7.
J. H.
Ferziger
and
M.
Peric
,
Computational Methods for Fluid Dynamics
, 3rd ed. (
Springer-Verlag
,
Berlin, Heidelberg
,
2002
).
8.
F.
Xiao
,
S.
Ii
, and
C.
Chen
, “
Revisit to the THINC scheme: A simple algebraic VOF algorithm
,”
Journal of Computational Physics
230
,
7086
7092
(
2011
).
This content is only available via PDF.