The problem of residual stresses in a structural member may play an important role in determining the oyerall actual stress distribution. A theoretical and experimental inves-tigation of residual stresses in a plate subjected to com-bined tensile and bending stresses are carried out in this paper. The basic concept adopted in the investigation is to apply known stresses on the loaded plate and then release a certian value of these stresses by making two single edge cracks. Known stresses are considered as residual stresses. The released strain on the relieved portion was measured using strain gages. A comparison between the results obtained using two single edge cracks method and two double edge cracks method is presented for the case of a plate under ten-sion. A good agreement between theoretical and experimental results is obtained for the plate subjected to combined load.
KHALIL, S., ASHOUR, N., & EL SAYED, M. (1993). INVESTIGATION OF RESIDUAL STRESSES IN A PLATE SUBJECTED TO COMBINED LOAD USING CRACK METHOD. International Conference on Aerospace Sciences and Aviation Technology, 5(ASAT CONFERENCE 4 - 6 May 1993, CAIRO), 243-251. doi: 10.21608/asat.1993.25626
MLA
S. A. KHALIL; N. M. ASHOUR; M. M. EL SAYED. "INVESTIGATION OF RESIDUAL STRESSES IN A PLATE SUBJECTED TO COMBINED LOAD USING CRACK METHOD", International Conference on Aerospace Sciences and Aviation Technology, 5, ASAT CONFERENCE 4 - 6 May 1993, CAIRO, 1993, 243-251. doi: 10.21608/asat.1993.25626
HARVARD
KHALIL, S., ASHOUR, N., EL SAYED, M. (1993). 'INVESTIGATION OF RESIDUAL STRESSES IN A PLATE SUBJECTED TO COMBINED LOAD USING CRACK METHOD', International Conference on Aerospace Sciences and Aviation Technology, 5(ASAT CONFERENCE 4 - 6 May 1993, CAIRO), pp. 243-251. doi: 10.21608/asat.1993.25626
VANCOUVER
KHALIL, S., ASHOUR, N., EL SAYED, M. INVESTIGATION OF RESIDUAL STRESSES IN A PLATE SUBJECTED TO COMBINED LOAD USING CRACK METHOD. International Conference on Aerospace Sciences and Aviation Technology, 1993; 5(ASAT CONFERENCE 4 - 6 May 1993, CAIRO): 243-251. doi: 10.21608/asat.1993.25626
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