Stability of liquid propellant missiles and spacecraft, controlled by autopilot system, is affected by propellant motions in tanks; response of propellant to sinusoidal forced motions, as translational, rotational, and bending oscillations of tank walls, is treated; velocity potential, free fluid surface displacement, pressure and velocity distribution in tanks, fluid forces, and moments were determined for small oscillations.
Theory of fluid oscillations in circular cylindrical ring tank partially filled with liquid
NASA -- Tech Note
1960
124 pages
Report
Englisch
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Axisymmetric vibrations of cylindrical-hemispherical tank partially filled with liquid
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