Effects of Repair Weld Residual Stresses on Wide-Panel Specimens Loaded in Tension

Author:

Dong P.1,Hong J. K.1,Zhang J.1,Rogers P.2,Bynum J.2,Shah S.3

Affiliation:

1. Battelle, 505 King Avenue, Columbus, OH 43201-2693

2. Marshall Space Flight Center, Huntsville, AL 35812

3. Lockheed Martin Manned Space Systems, Huntsville, AL 35812

Abstract

As a part of the welding fabrication procedure development for the next generation space shuttle external tank, aluminum-lithium wide-panel specimens were used to assess the interactions between repair weld residual stresses and external loading conditions. The detailed residual stress development in the wide panel specimens with a repair weld was analyzed using an advanced finite element procedure. External tension loading effects were then incorporated in the residual stress model to study the interactions between the residual stress field and external tensile loading. Wide-panel tensile tests were also performed to extract photo strain and strain-gage results. A good agreement between the finite element and experimental results was obtained. The results demonstrate that the presence of high tensile residual stresses within a repair weld has a drastic impact on the stress/strain distribution in the wide panel specimens subjected to external loading. Its implications on structural integrity are discussed in light of the wide-panel results. The effects of post-welding mechanical treatment such as planishing were also examined.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Safety, Risk, Reliability and Quality

Reference17 articles.

1. ABAQUS, 1994, User’s Manual, Version 5.3, Hibbitt, Karlson & Sorensen, Inc.

2. Anderson B. A. B. , 1978, “Thermal Stresses in a Submerged-Arc-Welded Joint Considering Phase Transformation,” ASME Journal of Engineering Materials and Technology, Vol. 100, pp. 356–362.

3. Brust, F. W., Dong, P., and Zhang, J., 1997, “A Constitutive Model for Welding Process Simulation Using Finite Element Methods,” Advances in Computational Engineering Science, S. N. Atluri and G. Yagawa, eds., pp. 51–56.

4. Dong, P., 1996a, Battelle Report No. G118803-01 to NASA Marshall Space Flight Center, Huntsville, AL.

5. Dong P. , et al., 1996b, “Effect of Weld Residual Stresses on Crack-Opening Area Analysis of Pipes for LBB Applications,” ASME PVP-Vol. 324, pp. 47–64.

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