TY - GEN
T1 - Experimental study of shock structure of particle-laden under expanded free jet
AU - Jain, Arihant
AU - Chen, Samuel
AU - Panerai, Francesco
AU - Villafane, Laura
N1 - Publisher Copyright:
© 2024 by the American Institute of Aeronautics and Astronautics, Inc.
PY - 2024
Y1 - 2024
N2 - An experimental investigation of under expanded particle-laden jet flows is conducted. The key parameter varied in the study is the mass loading ratio: the proportion of particle mass flow to air mass flow. A robust experimental setup is designed, calibrated, and built to produce repeatable data. Schlieren imagery with a horizontal knife edge and a high speed Chronos camera were used to analyze the shock structure of the resulting under expandedjet. Comparisons were made between Mach disc offset distance for unladen and laden flow. Contrary to literature, it is found that the Mach disc distance in particle-laden flow is dependent on both nozzle pressure ratio and mass loading ratio. Unladen data shows good agreement with literature and the Mach disc in laden flow is seen to move upstream with the addition of particles. Only qualitative comparisons are made to limited literature studies as mass loading ratios tested in this study, 0.5 – 2, were higher than those of literature: < 1. Further work is necessary to find a detailed empirical relationship between Mach disc offset distance, mass loading ratio, and nozzle pressure ratio.
AB - An experimental investigation of under expanded particle-laden jet flows is conducted. The key parameter varied in the study is the mass loading ratio: the proportion of particle mass flow to air mass flow. A robust experimental setup is designed, calibrated, and built to produce repeatable data. Schlieren imagery with a horizontal knife edge and a high speed Chronos camera were used to analyze the shock structure of the resulting under expandedjet. Comparisons were made between Mach disc offset distance for unladen and laden flow. Contrary to literature, it is found that the Mach disc distance in particle-laden flow is dependent on both nozzle pressure ratio and mass loading ratio. Unladen data shows good agreement with literature and the Mach disc in laden flow is seen to move upstream with the addition of particles. Only qualitative comparisons are made to limited literature studies as mass loading ratios tested in this study, 0.5 – 2, were higher than those of literature: < 1. Further work is necessary to find a detailed empirical relationship between Mach disc offset distance, mass loading ratio, and nozzle pressure ratio.
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U2 - 10.2514/6.2024-1981
DO - 10.2514/6.2024-1981
M3 - Conference contribution
AN - SCOPUS:85196816581
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -