Computational Methods for Membrane Structures
Markus Pagitz
Abstract
<>Balloon technology has steadily improved since the first flight by
the Montgolfier brothers in 1783. Nowadays the focus of development is
to create helium filled balloons that can stay at a height between 30
and 50 km for up to 100 days carrying a payload of several tonnes. This
kind of balloons will be used to create platforms for
telecommunication, intelligence or atmospheric research. The most
advanced program in developing this new generation of balloons is the
ULDB >Ultra Long Duration Balloon from NASA.
<>
These balloons have not much in common with the first small gas
balloons developed by Charles as their dimensions are with diameters of
more than one hundred meters - enormous. Furthermore the structure
itself is quite different from the first approaches. An ULDB is made of
a large number of lobes with reinforcing tendons at their seams that
meet at the top and bottom apexes. The advantage of a lobed balloon is
that the membrane between two tendons has a higher curvature than the
overall shape of the balloon wherefore the pressure forces can be
carried more efficiently to the meridional tendons by the membrane. Due
to the similarity between pumpkins and ULDB's the latter are often
called pumpkin balloons.> One of the problems that occurred
during the ascent of several pumpkin shaped balloons in the atmosphere
was that they did not deploy into the desired shape. The study of this
phenomenon is the goal of this thesis.
<>In order to build up numerical models which are able to simulate the
instability of balloons it is essential to develop the necessary
computational tools. As balloons are made out of very thin membranes,
and therefore susceptible to wrinkles, the first part of this thesis
deals with a novel finite element that can be used for the simulation
of wrinkled membranes. One of the properties of this new element is
that it can be used for heavily wrinkled structures without the
necessity of changing the material or deformation tensor at every
iteration step. The performance of this element is verified by showing
that it correctly represents the shearing of a thin rectangular
membrane, the bending of an inflated membrane cylinder with end loads,
and the form finding of catenoids and isotensoids.
>
The second part of this thesis looks at the stability of simple
lobed balloon structures. The structures under investigation are a
single truncated isotensoid and a stack of four truncated isotensoids
forming a kind of lobed cylinder. This lobed cylinder is an
axi-symmetric, idealised version of the lobed pumpkin balloons that
have occasionally deployed into anomalous, clefted configurations. By
studying these simplified structures it is possible to draw some
preliminary conclusions about general features of the behaviour of
lobed pumpkin balloons.
Key words: non-linear finite element, wrinkled membrane,
isotensoid, balloons, stability
[Cambridge University | CUED | Structures
Group | Geotechnical
Group]
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(last update 16 March 2005)