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Recent content by ParaDoc

  1. ParaDoc

    Thermal loading and spallation

    ...it seems to me a problem of thermal stresses developing at the interface of the deposited layer and the substrate during cooling down. To my knowledge there are a great many FEM-cotes which should be suitable for treating this problem. For example ABAQUS, MARC, ANSYS and the like. All what...
  2. ParaDoc

    Damping in rubber in Finite Element analysis

    ...see also my answer under "Finite Element Analysis Engineering" ...by the way I forgot to mention there that in case of having the "phase-lag" angle only at a given frequency and not for an relevant range ( ) it would be hard to estimate appropriately, because the...
  3. ParaDoc

    rayleigh damping instead of visco-el material?

    ...well, at least to my knowledge, if time integration is involved, you should rely on the so called "internal variable" approach of viscoelasticity. Here, the characteristic relaxation time constants of the given rubber governs the appropriate differential equations which have to be...
  4. ParaDoc

    Is there any data on the compressiv

    Shear Modulus roughly depends on the Shore-Hardness of the EPDM-grade. Let us assume you would take "ShA50" then the Shear Modulus is about 1MPa. The coefficient of thermal expansion is in the range of 120 to 180*10**(-6) 1/Kelvin depending on the compound (content of filler etc). best...
  5. ParaDoc

    Viscoelastic elastomers.

    ...well, if you need to have a rational procedure to optimise your "vibration-damping" device you first need to know the so called visco-elastic properties of the anticipated rubbery material in a sufficiently broad frequency range. This can be done easily by DMA measurements...
  6. ParaDoc

    Is there any data on the compressiv

    ... well, this may depend on which component (body) you are thinking about. For this to clarify I would suggest to read the following paper: "Load-compression Relationship of Rubber Unit" by P.B.LINDLEY; Journal of Strain Analysis Vol I No 3 1966 By the way I have in my lab an...
  7. ParaDoc

    Elastomer-metal Interface stresses

    ...in real life, on the interface between the metal and the rubber part, there is a small layer of "material" in which (on the rubber side!) the density of "molecular linkages" is much higher than in the rubber bulk itself. That means the stiffness of the rubber increases...
  8. ParaDoc

    SN curve for Natural Rubber

    ...well, you mean probably a kind of extrusion of the seal into a gap or the like? In that case the stain may be extraordinary large, but yielding will hardly occur, because you should keep in mind that you are dealing with a rubbery material. But what could take place is the following: the...
  9. ParaDoc

    o-ring fatigue

    . . . see also my suggestions under the THREAD: "S/N curve for Natural Rubber" !!!
  10. ParaDoc

    SN curve for Natural Rubber

    . . . as was already mentioned earlier in this thread, an attempt to quantify the service life of a rubber component (in the present case a seal)one is confronted with several limitations concerning a proper methodology and lack of knowledge on the fatigue processes of rubbers. Despite of these...
  11. ParaDoc

    o-ring fatigue

    . . . a good reference may be the book: How to design with rubber, Carl Hanser publisher edited by A.Gent This book gives an excellent overview on fatigue of rubber components etc.
  12. ParaDoc

    Is there any data on the compressiv

    ...there is a dump rule which relates shore-hardness to modulus of elasticity (irrespective of the rubber grade you are using). This rule tells us for example: 70 Shore A gives Youngs-Modulus roughly about 6MPa 55 Shore A gives Youngs-Modulus roughly about 3MPa 40 Shore A gives...
  13. ParaDoc

    Balloon deflation time

    ...no I do not! But there might be a more or less simple calculation method to determine the time needed to deflate a balloon of certain radius and "pressure gap" (outside pressure minus inside pressure). Because the driving force to squeeze out the contant of the balloon is the stress...

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