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International Conference on Aerospace Sciences and Aviation Technology
The present paper reports the results obtained from an experimental investigation carried out to study the dynamic responses of partially filled fluid tanks exhibiting a sloshing motion. A simple test rig has been developed to simulate such a phenomenon using a horizontal harmonic excitation system. Both cylindrical and spherical tank shapes have been considered. Mechanical Impedance Data were acquired for the different system and operational parameters. These include the fluid mass, tank size,doi:10.21608/asat.1985.26514 fatcat:fl4vs6f2rbbenhshblbkkkieei