Theory of shells , Membrane theory

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picovish
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I am working on a design of a spherical dome.

I tried to understand membrane theory with no success.Can anyone please help me with an clear explanation to derivation of membrane theory of shells.
 
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That is a pretty fuzzy question, but here are a few thoughts.

A typical membrane is a thin, flexible element like a rubber sheet. Thus a filled rubber balloon is a membrane shell.

Try drawing a Mohr's Circle for an element on the surface of a balloon. What you should find is that there is equal normal stress on all four sides of your stress block, no matter how it is oriented.

Does this get you started on membrane theory?
 
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yes,thank you.

yup , i agree. That is a fuzzy question.

I do understand the assumptions involved in membrane theory for designing a thin concrete shell structure. But i do not follow the derivation of it. I am doing my masters in structural engineering and I have never had classes in deferential geometry before.

( The following pages are not subject to copyrights.
  1. Theory of Plates and Shells by Stephen Timoshenko
  2. Published: 1940 )
why does the normal forces ,shear forces (pg 429 )bending and twisting moment have the term (1 - z/r) (pg 430)
Can you please explain pg 431.
Printed textbook page 429, Chapter 14 'Deformation of Shells Without Bending', showing section 104 definitions and equations for normal forces, shear forces and integrals with (1 - z/r) terms.

Printed textbook page 430 with text on bending and twisting moments in shells, two equations labelled (d) and (e) for M and M_xy, and Figure 212 showing a curved shell element and a radial cross-section (c).

Printed textbook page 431 with two columns of text and equations on deformation of shells without bending, including strain expressions with (1 - z/r) terms and the elongation formula e = (l1 - l)/l.

Printed textbook page 432 with typeset equations for stress components and force and moment resultants in shell theory, including N and M expressions and Eq. (253) and (254).
 
Attachments
  • Printed page of text with integral definitions for resultant forces N, N-xy, Q and related shell stress resultants, each integrating stress times (1 - z/r) over thickness from -h/2 to +h/2.
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There are a lot of video lectures for beam bending theory and classical plate bending theory, but there are almost none for theory of shells:nb)
 
Before tackling Timoshenko, let me suggest that you look at Den Hartog's Advanced Strength of Materials, McGraw-Hill, 1952, Ch III, "Membrane Stresses in Shells." On p. 78, Den Hartog addresses a spherical tank design problem, so this might be particularly relevant.

Specifically to your question from Timoshenko, "why does the normal forces ,shear forces (pg 429 )bending and twisting moment have the term (1 - z/r) (pg 430)," the answer is that Timoshenko is expressing the variation the stress through the thickness of the shell, much like assuming a linear variation of strain and stress through the depth of a beam in ordinary beam theory.
 
Generally speaking, an optimal design of a shell would ensure that stresses caused by the bending moments are small in comparison with the stresses caused by membrane forces. That would ensure that the shell would have good load bearing capacity and at the same time its thickness can be small compared with the shell overall span (as a result, the shell weight can be reduced). There is a special class of shells called shallow: the shell curvature is small, so it is "almost a plate" (so to say), but at the same time the distribution of internal stresses is such that the compression forces play the major role in the stress distribution under loading. You may want to have a look at the following webpage: http://members.ozemail.com.au/~comecau/quad_shell_shallow_shell.htm
(at the bottom of the page there is a reference to a book devoted, in particular, to that subject).
 
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I am going through the book "THIN SHELL CONCRETE STRUCTURES", Billington. It is quite good.
 
picovish said:
Thankyou
You are welcome. One of the reasons why I gave reference to that book is because it contains, in particular, working source codes that you may use and/or adapt for your problem (the theoretical background is also profound and presented accordingly).
 
Membrane theory derivation is not hard to follow at all. I think I did get a little rusty.

I will be soon designing an RC dome. Since it is going to be hemispherical ,there will not be any additional forces due to edge effects. But still I would like to know more about edge effects.

I am reading edge effects on shell structures. Can you suggest any literature for reading.
 
OldEngr63 said:
That is a pretty fuzzy question, but here are a few thoughts.

A typical membrane is a thin, flexible element like a rubber sheet. Thus a filled rubber balloon is a membrane shell.

Try drawing a Mohr's Circle for an element on the surface of a balloon. What you should find is that there is equal normal stress on all four sides of your stress block, no matter how it is oriented.

Does this get you started on membrane theory?

Thank you. The derivation was not tough to follow.

But I do have a question. Why does normal stress on all four sides of stress block has to be equal.

I think hoop stress and meridian stress will have different values.
 
Attachments
  • Handwritten-style typeset derivation for a spherical dome under self weight: membrane forces N-phi and N-theta from integrating p-phi and p-z, ending in N-phi = -aq/(1+cos phi) and an expression for N-theta.
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I am now doing an analysis on spherical domes with fixed edges. I am quite confused on applying the formula for forces and moments in a spherical shell due to edge forces. please help.
 
Can somebody please tell me what units these values in the formula are?
 
Attachments
  • Scanned page titled Table 6-1 Stresses and displacements resulting from edge effects, showing edge-force and edge-moment formulas for N phi, N theta, M phi, and the two displacement components in a spherical shell.
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