A SIMPLE METHOD FOR DETERMINATION OF RESIDUAL STRESSES USING DOUBLE-HOLE DRILLING TECHNIQUE | ||||
International Conference on Aerospace Sciences and Aviation Technology | ||||
Article 21, Volume 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, May 1991, Page 229-237 PDF (1.68 MB) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/asat.1991.25750 | ||||
View on SCiNiTO | ||||
Authors | ||||
M. O. HENDY1; M. M. EL-SAYED1; E. E. EL -SOALY2 | ||||
1Graduate Student and Assoc. Prof. in Mech. Design Dept., Faculty of Eng. and Tech., Mataria, Helwan University, Cairo. | ||||
2Prof. Gen. Chief of Mech. and Elasticity Dept., Military Technical College. | ||||
Abstract | ||||
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. | ||||
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