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Axisymmetric hydroelastic sloshing in a circular cylindrical container

Published online by Cambridge University Press:  04 July 2016

Helmut F. Bauer ,
James T. S. Wang  and
P. Y. Chen
Helmut F. Bauer
Affiliation:
Georgia Institute of Technology, Atlanta, Georgia
James T. S. Wang
Affiliation:
Georgia Institute of Technology, Atlanta, Georgia
P. Y. Chen
Affiliation:
Georgia Institute of Technology, Atlanta, Georgia
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Extract

The motion of liquid in the containers of a vehicle may have severe influence upon the stability of the vehicle. For this reason many authors have investigated the behaviour of liquid with a free surface due to various modes of excitation. In the earlier development of small vehicles, the frequencies of the elastic structures were relatively high compared to the propellant frequencies and the effect of their interaction could be neglected. With the increase of modern space vehicles this interaction of the propellant with the elastic structure is becoming a pronounced influence upon the design of the vehicle and its control system. This has some influence upon the stability and response behaviour of a large space vehicle, since the close grouping of propellant sloshing and structural frequencies around the control frequency of the vehicle creates continuous interaction during flight.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 76 , Issue 744 , December 1972 , pp. 704 - 712
Copyright
Copyright © Royal Aeronautical Society 1972 

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Footnotes

*

Professors, School of Engineering Science and Mechanics.

†

Formerly Research Assistant, School of Engineering Science and Mechanics, Georgia Institute of Technology; presently Senior Research Engineer, Babcock and Wilcox, Alliance, Ohio.

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