TY - JOUR
T1 - Simulating Melting-solidification of Lunar Regolith Particles Using Coupled CFD Methods
AU - Cavainolo, Brendon A.
AU - Torres-Figueroa, Andres
AU - Kinzel, Michael P.
N1 - Funding Information:
• This material is based upon work supported by the National Science Foundation Graduate Research Fellowship under Grant No. GR104853. • This material is based upon work supported by National Science Foundation grants OISE 1460045, OISE 1952523 and by the German Aerospace Center (DLR). • This material is based upon work supported by the National Aeronautics and Space Administration under Grant No. 80NSSC21M0309 issued through the NASA Office of STEM Engagement • The UCF College of Engineering and Computer Science Graduate Dean’s Fellowship
Publisher Copyright:
© 2022 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2022
Y1 - 2022
N2 - Lunar exploration endeavours, such as the Artemis program, demand the study of the behaviour of lunar dust. Lunar landing scenarios involve high-enthalpy interactions with lunar regolith. This work proposes that regolith particles experience a melting mechanism, making a “sticky” partially melted liquid outer layer, leading to unique interactions between regolith and structures on the lunar surface. (Alternate to these next few sentences: An analytical source flow model was used to estimate the flow conditions a certain distance away from a plume. The results for the analytical model were used as boundary conditions for a Computational fluid dynamics (CFD) simulation. The simulation was set up using the Eulerian volume-of-fluid (VOF) method and was used to simulate the melting-solidification of the particle as it interacts with a structure. The VOF model extends one formulated for sand ingestion into aircraft but has been uniquely adapted to study partially-melted regolith impacts. The VOF method was used to capture the solid to partial solid/liquid phase change dynamics of the melting regolith particles. The final paper presents novel studies elucidating dynamic properties of melting regolith. Simulations involve initializing a regolith particle at ambient conditions and the surrounding fluid to rocket plume conditions. Time-varying temperature, melting, aerodynamic character, and shape are extracted. Non-dimensional variables, including Reynolds, Weber, and Ohnesorge numbers, are explored. The outcome of this paper will provide guidance relevant to the fouling of surfaces from partially melted regolith during landings.
AB - Lunar exploration endeavours, such as the Artemis program, demand the study of the behaviour of lunar dust. Lunar landing scenarios involve high-enthalpy interactions with lunar regolith. This work proposes that regolith particles experience a melting mechanism, making a “sticky” partially melted liquid outer layer, leading to unique interactions between regolith and structures on the lunar surface. (Alternate to these next few sentences: An analytical source flow model was used to estimate the flow conditions a certain distance away from a plume. The results for the analytical model were used as boundary conditions for a Computational fluid dynamics (CFD) simulation. The simulation was set up using the Eulerian volume-of-fluid (VOF) method and was used to simulate the melting-solidification of the particle as it interacts with a structure. The VOF model extends one formulated for sand ingestion into aircraft but has been uniquely adapted to study partially-melted regolith impacts. The VOF method was used to capture the solid to partial solid/liquid phase change dynamics of the melting regolith particles. The final paper presents novel studies elucidating dynamic properties of melting regolith. Simulations involve initializing a regolith particle at ambient conditions and the surrounding fluid to rocket plume conditions. Time-varying temperature, melting, aerodynamic character, and shape are extracted. Non-dimensional variables, including Reynolds, Weber, and Ohnesorge numbers, are explored. The outcome of this paper will provide guidance relevant to the fouling of surfaces from partially melted regolith during landings.
UR - https://www.scopus.com/pages/publications/85167576931
UR - https://www.scopus.com/pages/publications/85167576931#tab=citedBy
M3 - Conference article
AN - SCOPUS:85167576931
SN - 0074-1795
VL - 2022-September
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
T2 - 73rd International Astronautical Congress, IAC 2022
Y2 - 18 September 2022 through 22 September 2022
ER -