Submitting Campus
Daytona Beach
Department
Applied Aviation Sciences
Document Type
Article
Publication/Presentation Date
1-4-2024
Abstract/Description
This study presents the results of a parabolic flight experiment to study the sloshing dynamics of the magneto-active propellant management device experiment. This device utilizes a magnetoactive membrane and magnets located external to the tank to effectively damp the liquid free surface motion. This research work establishes a benchmark with sloshing analytical formulation and sensor calibration methods that can be used to characterize future research parabolic flights while providing important environmental profiles measured during flight, such as accelerations, pitch angle, velocity, temperature, total volatile content, carbon dioxide, relative humidity, magnetic field, and radiation. Correlation between these flight variables and the sloshing experiment are suggested to improve suppression of sloshing. Preliminary postflight analysis suggests a close correlation between high peaks of carbon dioxide and total volatile compound levels during the parabolas – levels sustained for up to one hour combined during cruise in some parabolic flights.
Publication Title
AIAA Scitech 2024 Forum
DOI
https://doi.org/10.2514/6.2024-0083
Publisher
American Institute of Aeronautics and Astronautics
Scholarly Commons Citation
Llanos, P. J., Gangadharan, S., & Crosby, K. (2024). Experimental Environmental Profiles and Sloshing Dynamics Aboard Zero-G Aircraft. AIAA Scitech 2024 Forum, (). https://doi.org/10.2514/6.2024-0083
Included in
Aerodynamics and Fluid Mechanics Commons, Aeronautical Vehicles Commons, Electro-Mechanical Systems Commons