Further studies of liquid sloshing in rocket propellant tanks Final report, 25 Mar. 1961 - 31 Dec. 1965

Liquid sloshing and dynamics in rocket propellant tanks annotated bibliography with abstract

Refracting profiles and generalized holodiagrams

The recently developed concept of refracting profiles and that of refraction holodiagrams are combined so that the classical Abramson holodiagrams can be generalized taking into account a wider class of wave fronts and refraction at an interface, whenever regions of caustics are avoided. These holodiagrams are obtained as envelopes of specific families of Cartesian Ovals with an appropriate parametrization. Classical and reflecting holodiagrams are particular cases of this class. Several of the properties of the classical holodiagrams are shared by their richer generalized versionsComment: 12 pages, 7 figure

MEASUREMENTS OF LIQUID DAMPING PROVIDED BY RING BAFFLES IN CYLINDRICAL TANKS

Damping effect of flat ring baffles on liquid sloshing in partially filled cylindrical tank

Longitudinal vibration of ring stiffened cylindrical shells containing liquids Technical report no. 7

Longitudinal vibration of ring stiffened cylindrical shells containing liquids for application to liquid fueled space vehicle booster

Liquid Sloshing in 45 Deg Sector Compartmented Cylindrical Tanks

Liquid sloshing in 45-deg sector compartmented cylindrical tank

Pressures on ring baffles. Damping coefficients for mechanical models of liquid sloshing Quarterly progress report no. 16, 1 Jan. - 31 Mar. 1965

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 tan

Sloshing studies Quarterly progress report no. 16, 1 Jan. - 31 Mar. 1965

Harmonic analysis of pressure data for solid and perforated baffle plates of fuel tank

Fuel sloshing studies Quarterly progress report no. 15, 1 Oct. - 31 Dec. 1965

Pressure distribution on single solid ring baffle due to fuel sloshing in cylindrical tan

Some Notes on Liquid Sloshing in Compartmented Cylindrical Tanks Technical Report No. 1

Frequencies and total force response in rigid cylindrical tanks comparted into sectors by vertical walls and excited in translation to study liquid sloshin

Light-in-flight recording. 5: Theory of slowing down the faster-than-light motion of the light shutter

Light-in-flight recording by holography uses a picosecond pulse for the reference beam, which like a sheet of light intersects the hologram plate and produces a sensitivity area that with a speed faster than light moves over the plate like a light shutter. If, however, the front of the reference pulse by diffraction in a grating is tilted relative to its direction of motion, the velocity of the light shutter can be slowed down resulting in increased recording time. The practical result using a reflection grating was a true recording that corresponded to a time compression of two to one. To minimize distortions of the recorded pulse shape we studied intersections that are identical for apparent (ellipsoidal) and true (spheroidal) wavefronts