salmon2
Materials
- Feb 1, 2008
- 360
I meant to post here, but accidently posted it first in the ASTM forum. Anyway.
My question is about how to calculate collapse pressure of steel casing or tubing including imperfection effects, such as tolerance, residual stress, etc.
I am using the paper "A new empirical formula for collapse resistance of commercial casing" by T. Tamano, T. Mimaki and S. Yanaimoto. This empirical model included the effect of tolerances, residual stress and seems pretty good. The formula are:
1) Elastic collapse pressure
Pea=2*E/(1-v^2)/(D/t)/(D/t-1)^2
where E is elastic modulus, v possion ration, D Outer diameter and t wall thickness
2) yield collapse pressure
Pyie=2*YS*(D/t-1)/(D/t)^2*(1+1.47/(D/t-1))
where YS is anxial yield strength
3) imperfection factor
H=0.0808*u(%) + 0.00114*e(%) - 0.1412RS/YS
where u is ovality in % and e eccentricity in % and RS is circumferential residual stress at the insider surface of tubing
4) The empirical collapse pressure will be
P=0.5*(Pea+Pyie)-(0.25(Pea-Pyie)^2+Pea*Pyie*H)^0.5
The applicable range of D/t will be between 10 ~ 26.
The tubing I work with is either API 5CT or 5L, seamless or ERwelded. The tolerance I order is either OD/wall controlled or ID/wall depending the tubing manufacturing process. The problems I have are how to calculate the u, e and RS.
1) on the ovality u, people already discussed somewhere before, the prevailing one will be u = (Dmax-Dmin)/Davg. Say the OD tol is +/-1%, then u = 2%. This single imperfection will decrease the pressure calculation as above by 30%! my question is this seems overconservative and underestimate the collapse pressure a lot compared with testing? I am thinking either tube manufacturing did not use up the full range of OD tolerance or the calculation of u should be restricted at one cross section and then used the max u only because where is mostly the spot to collapse and the max u from each cross section should be much smaller than theoretical limit, 2% in this case. I would like to hear your expertise explanation on this.
2) on eccentricity, e, people use e = (t_max-t_min)/t_avg. Say the wall thickness tolerace is +/-10%, then e equals to 20%. Again is this overconservative or should be restricted to one cross section only…?
3) how to measure the residual stress on the internal surface only? Is there any way I can calculate it? I know I can cut a ring longitudinally and compare the OD before and after cutting, but that is the effective residual stress throughout the wall thickness and it varied a lot between different heats, roughly same chemistry and heat treatment.
4) finally, is there other better models available including the imperfection effect people know of?
My question is about how to calculate collapse pressure of steel casing or tubing including imperfection effects, such as tolerance, residual stress, etc.
I am using the paper "A new empirical formula for collapse resistance of commercial casing" by T. Tamano, T. Mimaki and S. Yanaimoto. This empirical model included the effect of tolerances, residual stress and seems pretty good. The formula are:
1) Elastic collapse pressure
Pea=2*E/(1-v^2)/(D/t)/(D/t-1)^2
where E is elastic modulus, v possion ration, D Outer diameter and t wall thickness
2) yield collapse pressure
Pyie=2*YS*(D/t-1)/(D/t)^2*(1+1.47/(D/t-1))
where YS is anxial yield strength
3) imperfection factor
H=0.0808*u(%) + 0.00114*e(%) - 0.1412RS/YS
where u is ovality in % and e eccentricity in % and RS is circumferential residual stress at the insider surface of tubing
4) The empirical collapse pressure will be
P=0.5*(Pea+Pyie)-(0.25(Pea-Pyie)^2+Pea*Pyie*H)^0.5
The applicable range of D/t will be between 10 ~ 26.
The tubing I work with is either API 5CT or 5L, seamless or ERwelded. The tolerance I order is either OD/wall controlled or ID/wall depending the tubing manufacturing process. The problems I have are how to calculate the u, e and RS.
1) on the ovality u, people already discussed somewhere before, the prevailing one will be u = (Dmax-Dmin)/Davg. Say the OD tol is +/-1%, then u = 2%. This single imperfection will decrease the pressure calculation as above by 30%! my question is this seems overconservative and underestimate the collapse pressure a lot compared with testing? I am thinking either tube manufacturing did not use up the full range of OD tolerance or the calculation of u should be restricted at one cross section and then used the max u only because where is mostly the spot to collapse and the max u from each cross section should be much smaller than theoretical limit, 2% in this case. I would like to hear your expertise explanation on this.
2) on eccentricity, e, people use e = (t_max-t_min)/t_avg. Say the wall thickness tolerace is +/-10%, then e equals to 20%. Again is this overconservative or should be restricted to one cross section only…?
3) how to measure the residual stress on the internal surface only? Is there any way I can calculate it? I know I can cut a ring longitudinally and compare the OD before and after cutting, but that is the effective residual stress throughout the wall thickness and it varied a lot between different heats, roughly same chemistry and heat treatment.
4) finally, is there other better models available including the imperfection effect people know of?