Classical diffuse interface methods for non-equilibrium formulations of two-phase flows are not capable of preserving interface-thickness. Furthermore, when coupled with shock …
A Sukumaran, B Boyd, D Jarrahbashi - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
Depending on the mission and flight trajectory hypersonic vehicles must travel through rain droplets and clouds of ice particles at various altitudes mainly during take-off or landing. The …
Using detailed 2D axisymmetric numerical simulations, we investigate the deformation and kinematics of a 10 µm acetone droplet impacted by a Mach 2.4 shock wave. The simulations …
S Agee, C Young, V Duke-Walker, M Paudel… - AIAA SCITECH 2025 …, 2025 - arc.aiaa.org
Multiphase detonations with aerosolized liquid fuel are a complex multi-scale multi-physics problem. The development of detonation propulsion devices utilizing liquid fuels requires an …