Shock structures and post-impact jetting in hypervelocity droplet impingement

Abstract The shock dynamics resulting from high-speed droplet impingement on a rigid surface are investigated employing high-resolution schlieren imaging and numerical simulations based on the five-equation model. A key finding is that, in contrast to the common emphasis on jetting-induced dynamics, the long-time shock morphology is governed not by explosive shocks generated during jetting, but rather by the reflection of the droplet’s own shock wave off the solid wall. The resulting shock structure is found to be robust across a wide range of densities and breakup states, and its evolution is shown to depend primarily on the impact Mach number. Axisymmetric and 3D simulations both capture the wall-reflected envelope with high fidelity, despite shared limitations in modeling post-impact jetting dynamics. The presented results clarify the physical mechanisms shaping post-impingement shock evolution and highlight the modeling trade-offs involved in capturing jet-driven transients. This paper provides a unique experimental and numerical dataset that can be used as a reference for future studies.

Authors

Institutions

Publication Details

Journal
Shock Waves
Published
2026-10-17
DOI
https://doi.org/10.1007/s00193-026-01292-2
Primary Topic
Fluid Dynamics and Heat Transfer
Type
article
Field-Weighted Citation Impact
0.00

Funders

Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Shock structures and post-impact jetting in hypervelocity droplet impingement

Christoph E Brehm, Alex R. Dworzanczyk, Michael A. Libeau, Nick J. Parziale et al.
Shock Waves
Fluid Dynamics and Heat Transfer
article

Shock structures and post-impact jetting in hypervelocity droplet impingement

Christoph E Brehm, Alex R. Dworzanczyk, Michael A. Libeau, Nick J. Parziale, Manuel Viqueira-Moreira, Jett D. Langhorn, J. B. Middlebrooks
article en

Abstract

Abstract The shock dynamics resulting from high-speed droplet impingement on a rigid surface are investigated employing high-resolution schlieren imaging and numerical simulations based on the five-equation model. A key finding is that, in contrast to the common emphasis on jetting-induced dynamics, the long-time shock morphology is governed not by explosive shocks generated during jetting, but rather by the reflection of the droplet’s own shock wave off the solid wall. The resulting shock structure is found to be robust across a wide range of densities and breakup states, and its evolution is shown to depend primarily on the impact Mach number. Axisymmetric and 3D simulations both capture the wall-reflected envelope with high fidelity, despite shared limitations in modeling post-impact jetting dynamics. The presented results clarify the physical mechanisms shaping post-impingement shock evolution and highlight the modeling trade-offs involved in capturing jet-driven transients. This paper provides a unique experimental and numerical dataset that can be used as a reference for future studies.

Shock WavesVol. 36(3)
Stevens Institute of Technology (US), Naval Surface Warfare Center (US), University of Maryland, College Park (US)
Office of Naval Research
Openalex Percentile: Top 18%
Fluid Dynamics and Heat Transfer
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.