An approximate nonlinear analysis of the stability of sloshing modes under transla- tional and rotational excitation
Nonlinear analysis of sloshing mode stability under translational and rotational excitation
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Nonlinear analysis of sloshing mode stability under translational and rotational excitation
Equations for dynamic behavior of liquid propellants sloshing in mobile tanks of arbitrary shape
Sloshing forces and moments on cylindrical tank - integration of nonlinear force equations
Capacitance sensors for measuring liquid propellant sloshing in space vehicle fuel tanks
Computer program applying hydrodynamic equations to describe sloshing of liquid propellant in mobile tank having rotational symmetry
Testing of cantilevered flexible, hinged, and slamming baffles by subjection to sinusoidal variation in water far from free surface - effect on tank sloshing
Flexible baffle effect on nature and magnitude of damping and sloshing motions of liquid propellants over wide range of conditions
Stability boundaries for planar or nonplanar sloshing in spherical tanks
Nonlinear lateral sloshing in rigid containers
Frequencies and total force response in rigid cylindrical tanks comparted into sectors by vertical walls and excited in translation to study liquid sloshing
Harmonic analysis of pressures on ring baffles, force measurements for solid and perforated ring baffles, and inertia damping coefficient for model of liquid sloshing - fuel tank
Equation for predicting liquid slosh damping ring baffle in cylindrical fuel tank
Action of pressures and loading forces on ring baffle under sloshing conditions
This paper describes a method for determining the optimum baffle configuration for suppressing excessive propellant sloshing in the tanks of a large launch vehicle. The optimum geometry for a baffle system is considered to be the one with the least mass which is capable of providing the necessary damping. The analysis considers a cylindrical tank and a baffle system made up of several flat ring baffles mounted horizontally. The basic assumptions are discussed and derivations given of the equations necessary to predict the optimum baffle configuration consistent with adequate strength. Numerical results are presented graphically, and some general conclusions are drawn.
Liquid sloshing and dynamics in rocket propellant tanks annotated bibliography with abstracts
Transfer function approximations for large highly coupled flexible body launch vehicles with liquid fuel slosh
Liquid sloshing in cylindrical and spherical tanks
Pressure distribution on single solid ring baffle due to fuel sloshing in cylindrical tank