BAR:Extension of the rod under the axial pull, \(\delta l = \frac{{PL}}{{\left( {\frac{\PI }{4}} \right) \times \left( {{d_1}{d_2}} \right) \times E}}\)whereP = load appliedL = LENGTH of the barE = MODULUS of elasticityd1 and d2 are the tapered diameters\(\delta = \frac{{4PL}}{{\pi {d_1}{d_2}E}}\)Calculation: Elongation in bar, using standard formula is given by,\({\rm{\Delta }}L = \frac{{4PL}}{{\mu {D_1}{D_2}E}}\)P = 12 kNL = 450 mmD1 = 36 mmD2 = 18 mmE = 2 × 105 N/mm2\({\rm{\Delta }}L = \frac{{4\; \times \;\left( {12\; \times \;{{10}^3}} \right)\; \times \;450}}{{\pi\; \times \;36\; \times \;18\; \times \;2\; \times \;105}}\)\({\rm{\Delta }}L = \frac{1}{{6\pi }}\;mm\)

"> BAR:Extension of the rod under the axial pull, \(\delta l = \frac{{PL}}{{\left( {\frac{\PI }{4}} \right) \times \left( {{d_1}{d_2}} \right) \times E}}\)whereP = load appliedL = LENGTH of the barE = MODULUS of elasticityd1 and d2 are the tapered diameters\(\delta = \frac{{4PL}}{{\pi {d_1}{d_2}E}}\)Calculation: Elongation in bar, using standard formula is given by,\({\rm{\Delta }}L = \frac{{4PL}}{{\mu {D_1}{D_2}E}}\)P = 12 kNL = 450 mmD1 = 36 mmD2 = 18 mmE = 2 × 105 N/mm2\({\rm{\Delta }}L = \frac{{4\; \times \;\left( {12\; \times \;{{10}^3}} \right)\; \times \;450}}{{\pi\; \times \;36\; \times \;18\; \times \;2\; \times \;105}}\)\({\rm{\Delta }}L = \frac{1}{{6\pi }}\;mm\)

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A mild steel bar of length 450 mm tapers uniformly. The diameters at the ends are 36 mm and 18 mm, respectively. An axial load of 12kN is applied on the bar. E = 2 × 105 N/mm2. The elongation of the bar will be

Materials Science Stress Strain in Materials Science . 7 months ago

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Concept:Deflection (\(\Delta\)) of circular Tapering BAR:Extension of the rod under the axial pull, \(\delta l = \frac{{PL}}{{\left( {\frac{\PI }{4}} \right) \times \left( {{d_1}{d_2}} \right) \times E}}\)whereP = load appliedL = LENGTH of the barE = MODULUS of elasticityd1 and d2 are the tapered diameters\(\delta = \frac{{4PL}}{{\pi {d_1}{d_2}E}}\)Calculation: Elongation in bar, using standard formula is given by,\({\rm{\Delta }}L = \frac{{4PL}}{{\mu {D_1}{D_2}E}}\)P = 12 kNL = 450 mmD1 = 36 mmD2 = 18 mmE = 2 × 105 N/mm2\({\rm{\Delta }}L = \frac{{4\; \times \;\left( {12\; \times \;{{10}^3}} \right)\; \times \;450}}{{\pi\; \times \;36\; \times \;18\; \times \;2\; \times \;105}}\)\({\rm{\Delta }}L = \frac{1}{{6\pi }}\;mm\)

Posted on 02 Nov 2024, this text provides information on Materials Science related to Stress Strain in Materials Science. Please note that while accuracy is prioritized, the data presented might not be entirely correct or up-to-date. This information is offered for general knowledge and informational purposes only, and should not be considered as a substitute for professional advice.

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