TY - GEN
T1 - Particle-laden high-speed flows over a blunted cone
AU - Liu, Qiong
AU - Karpuzcu, Irmak T.
AU - Marayikkottu, Akhil V.
AU - Levin, Deborah A.
N1 - We thank the computational resource from TACC Long-term tape Archival Storage (Ranch), TACC Dell/Intel Knights Landing, Skylake System (Stampede2) and Purdue Anvil CPU with the project number PHY220046.
PY - 2023
Y1 - 2023
N2 - The ubiquitous particle-laden flows affecting the performances of flight vehicles, such as erosion and cratering on the vehicle surface, have been well-recognized. However, the dynamics of particle-laden high-speed flow have yet to be fully understood. This study examines the particle dynamics in an air over an axisymmetric blunted-cone configuration at Mach numbers 6, 9, and 14 and an altitude of 45km. The direct simulation Monte Carlo (DSMC) method is employed to obtain flow solutions in rarefied flow regimes. A one-way coupled Lagrangian particle methodology with an inelastic rough hard sphere model is developed to examine particle-laden flow dynamics for the particle size range of 0.01μm ≤ dp≤ 2μm. The results showed the bow shocks affect the light particle dynamics, including trajectory deflecting upward, streamwise velocity deceleration, and quick temperature rise. In comparison, the effects on the heavy particles are negligible. A dust-free region is observed along the body of the blunted cone for light particles of dp= 0.02μm. Heavy particles dp= 0.2μm have a broad impact region where the post-collisional particles are presenting.
AB - The ubiquitous particle-laden flows affecting the performances of flight vehicles, such as erosion and cratering on the vehicle surface, have been well-recognized. However, the dynamics of particle-laden high-speed flow have yet to be fully understood. This study examines the particle dynamics in an air over an axisymmetric blunted-cone configuration at Mach numbers 6, 9, and 14 and an altitude of 45km. The direct simulation Monte Carlo (DSMC) method is employed to obtain flow solutions in rarefied flow regimes. A one-way coupled Lagrangian particle methodology with an inelastic rough hard sphere model is developed to examine particle-laden flow dynamics for the particle size range of 0.01μm ≤ dp≤ 2μm. The results showed the bow shocks affect the light particle dynamics, including trajectory deflecting upward, streamwise velocity deceleration, and quick temperature rise. In comparison, the effects on the heavy particles are negligible. A dust-free region is observed along the body of the blunted cone for light particles of dp= 0.02μm. Heavy particles dp= 0.2μm have a broad impact region where the post-collisional particles are presenting.
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U2 - 10.2514/6.2023-2301
DO - 10.2514/6.2023-2301
M3 - Conference contribution
AN - SCOPUS:85196827702
SN - 9781624106996
T3 - AIAA SciTech Forum and Exposition, 2023
BT - AIAA SciTech Forum and Exposition, 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2023
Y2 - 23 January 2023 through 27 January 2023
ER -