One of the most common semi-distructive methods for determination of re-sidual stresses in plates is the drilling hole method. In this method, a strain rosette or a set of strain gauges are usually used to measure the relaxed strains induced due to drilling of a central hole. The present work *atroduces a new simple method for determination of residual stresses in unigxially stressed plates using double hole technique. Optimum dimen-sions for hole diameter and hole spacing, associated with a specific strain-gauge length, are determined. A constant relating the residual stress and the relaxed strain in a plate is obtained. Three different plate materials are considered; steel, laminated brass and aluminum. An experimental work is done to verify the theoretical analysis. For the stated plate materials, the experimental and theoretical results are in a good agreement.
HENDY, M., EL-SAYED, M., & EL -SOALY, E. (1991). A SIMPLE METHOD FOR DETERMINATION OF RESIDUAL STRESSES USING DOUBLE-HOLE DRILLING TECHNIQUE. International Conference on Aerospace Sciences and Aviation Technology, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), 229-237. doi: 10.21608/asat.1991.25750
MLA
M. O. HENDY; M. M. EL-SAYED; E. E. EL -SOALY. "A SIMPLE METHOD FOR DETERMINATION OF RESIDUAL STRESSES USING DOUBLE-HOLE DRILLING TECHNIQUE". International Conference on Aerospace Sciences and Aviation Technology, 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, 1991, 229-237. doi: 10.21608/asat.1991.25750
HARVARD
HENDY, M., EL-SAYED, M., EL -SOALY, E. (1991). 'A SIMPLE METHOD FOR DETERMINATION OF RESIDUAL STRESSES USING DOUBLE-HOLE DRILLING TECHNIQUE', International Conference on Aerospace Sciences and Aviation Technology, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), pp. 229-237. doi: 10.21608/asat.1991.25750
VANCOUVER
HENDY, M., EL-SAYED, M., EL -SOALY, E. A SIMPLE METHOD FOR DETERMINATION OF RESIDUAL STRESSES USING DOUBLE-HOLE DRILLING TECHNIQUE. International Conference on Aerospace Sciences and Aviation Technology, 1991; 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO): 229-237. doi: 10.21608/asat.1991.25750
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