Tanks containing liquid propellants for rocket engines can be considered as shells whose thin walls are surfaces of revolution. Such surfaces result from a plane curve which rotates about some straight line lying in the plane which contains the curve. The structural analysis of tanks is presented here by using Roark’s formulas for stress and strain. Loads due to propellant sloshing and slosh-suppression devices are also discussed.
Tanks for Propellants
Springer Aerospace Techn.
27.09.2020
94 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Prediction of gas-core vortices during draining of liquid propellants from tanks
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