TY - GEN
T1 - High-Speed Multiphase Verification and Code-to-Code Comparison
AU - Sayad, Andrew
AU - Rabinovitch, Jason
AU - Viqueira-Moreira, Manuel
AU - Patel, Monal
AU - Brehm, Christoph
AU - Sarker, Anik
AU - Jarrahbashi, Dorrin
N1 - Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2024
Y1 - 2024
N2 - Multiphase flow is commonplace in a variety of engineering and scientific applications. This paper presents a variety of one and two-dimensional compressible multiphase test case problems to document and analyze the differences between five different CFD frameworks. The test problems chosen include 1D problems: a multiphase shocktube problem, a Sedov blastwave problem, and a material interface advection problem. The 2D problems considered include shock water-cylinder interactions at shock Mach numbers of 1.47, 2.4, and 10, as well as a water-cylinder impingement problem (water-cylinder impacting a rigid wall). Mach 2.4 shock water-cylinder results are compared against experimental shadowgraph images. These test cases are solved on a coarse and refined mesh grid to test the solution’s sensitivity with respect to mesh resolution. Differences between the solutions are noted and discussed, and suggestions for future research and test cases are included.
AB - Multiphase flow is commonplace in a variety of engineering and scientific applications. This paper presents a variety of one and two-dimensional compressible multiphase test case problems to document and analyze the differences between five different CFD frameworks. The test problems chosen include 1D problems: a multiphase shocktube problem, a Sedov blastwave problem, and a material interface advection problem. The 2D problems considered include shock water-cylinder interactions at shock Mach numbers of 1.47, 2.4, and 10, as well as a water-cylinder impingement problem (water-cylinder impacting a rigid wall). Mach 2.4 shock water-cylinder results are compared against experimental shadowgraph images. These test cases are solved on a coarse and refined mesh grid to test the solution’s sensitivity with respect to mesh resolution. Differences between the solutions are noted and discussed, and suggestions for future research and test cases are included.
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U2 - 10.2514/6.2024-4479
DO - 10.2514/6.2024-4479
M3 - Conference contribution
AN - SCOPUS:85204212792
SN - 9781624107160
T3 - AIAA Aviation Forum and ASCEND, 2024
BT - AIAA Aviation Forum and ASCEND, 2024
T2 - AIAA Aviation Forum and ASCEND, 2024
Y2 - 29 July 2024 through 2 August 2024
ER -