EFFECT OF SHELL ENDS ON THE CONTACT PROBLEMS | ||||
The International Conference on Applied Mechanics and Mechanical Engineering | ||||
Article 10, Volume 2, 1st Conference on Applied Mechanical Engineering., May 1984, Page 145-156 PDF (2.3 MB) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/amme.1984.49563 | ||||
View on SCiNiTO | ||||
Authors | ||||
N. EL. BEKHET1; Z. Z. MOMEH2; F. EL-SHERIF3 | ||||
1Graduate student, Dept. of Machine Design, Faculty of Engineering and Technology, Mataria-Cairo. | ||||
2Col.Dr. Dept. of Mechanics and Elasticity, Military Technical college, Cairo. | ||||
3Professor, Dept. of Machine Design, Faculty of Engineering and Technology, Mataria-Cairo. | ||||
Abstract | ||||
The effect of shell ends on the contact problems of saddle supporting cylindrical shell is solved using the semi-bending theory of shells. The saddle / cylinder interface pressure and the stress distributions are found for different saddle angles, for both welded saddle and not welded saddle. The min. distance of the saddle position from the shell end is found such that the end has no effect on the stress at the saddle positions. The circumferential stresses at the plane of middle profile of the saddle are found experimentally using strain gauge. The experimental results are in good agreement with those obtained from numerical analysis. | ||||
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