Shell element transverse shear stresses calculation in ABAQUS VUMAT

Hi Everyone,

I've couple of quick questions:

1) I am planning to use ABAQUS 2D shell formulation (S4R) to estimate
3D state of stress (to reduce the computational cost). I've read several articles to estimate the
transverse shear stresses once the in-plane stresses are known by
integrating the 3D equilibrium equations. This is, of course, easily
done, if we have closed form solutions for in-plane stresses:

sigma_xz,z = - (sigma_xx,x + sigma_xy,y)
sigma_yz,z = - (sigma_xy,x + sigma_yy,y)

How do I estimate transverse shear stresses using ABAUAS VUMAT, when I
only know the in-plane stresses at one integration point in the element
(in case of S4R) in VUMAT? Else, is there any possibility to transfer/estimate the transverse shear strains within the VUMAT?

 

2) In my analysis, I will use progressive failure analysis, where
transverse stiffness cannot be kept constant in the analysis (I read in
ABAQUS manual, we cannot change the transverse stiffness. Is there any
possibility to control transverse stiffness, within VUMAT, in case of shell elements?

Thank you for your help,
Nagesh


nepolean.r's picture

same query - how to estimate TRANSVERSE SHEAR STIFFNESS in VUMAT

Graduate Student
Univ of Cincinnati


nepolean.r's picture

same query - how to estimate TRANSVERSE SHEAR STIFFNESS in VUMAT

Hi ,

I am trying to solve for S4R elements with a VUMAT (compressible hyperelastic mooney rivlin material model).

I have the C10, C01 and D1 parameters.

this needs transverse shear stiffness to be supplied in input using the keyword *TRANSVERSE SHEAR STIFFNESS   

can you kindly help me with some idea on how to proceed with my problem.

thanks a lot

Nepolean