Numerical Investigation of Droplet Aerobreakup and Impingement Experiments at Mach 5
Author:
Affiliation:
1. University of Maryland at College Park
2. Stevens Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-4251
Reference25 articles.
1. The physics of aerobreakup. II. Viscous liquids
2. A ghost fluid method for compressible reacting flows with phase change
3. A comparison of higher-order finite-difference shock capturing schemes
4. A positivity-preserving high-order weighted compact nonlinear scheme for compressible gas-liquid flows
5. Validation of a High-Order Diffuse Interface Multi-Phase Method for High-Speed Droplet Shock Interaction and Impingement
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