UNIT-01. SIMPLE STRESSES & STRAINS Lecture Number - 06 Prof. S.C.SADDU MECHANICAL DEPARTMENT SIT LONAVALA Strength of Materials Agenda • To study temperature stresses and temperature strain Strength of Materials Thermal Stresses • A temperature change results in a change in length or thermal strain. There is no stress associated with the thermal strain unless the elongation is restrained by the supports. • Treat the additional support as redundant and apply the principle of superposition. PL T T L P AE thermal expansion coef. • The thermal deformation and the deformation from the redundant support must be compatible. T P 0 T P 0 P AE T T L PL 0 AE Strength of Materials P E T A Temperature stresses • Extension in bar due to raise in temperature is, L= *T *L • Temperature Strain is, = *T • Temperature Stress developed is, = *E*T Strength of Materials Example: 1 A steel tube having an external diameter of 36 mm and an internal diameter of 30 mm has a brass rod of 20 mm diameter inside it, the two materials being joined rigidly at their ends when the ambient temperature is 18 0C. Determine the stresses in the two materials: (a) when the temperature is raised to 68 0C (b) when a compressive load of 20 kN is applied at the increased temperature. • For brass: Modulus of elasticity = 80 GN/m2; Coefficient of expansion = 17 x 10 -6 /0C • For steel: Modulus of elasticity = 210 GN/m2; Coefficient of expansion = 11 x 10 -6 /0C Strength of Materials 30 Brass rod 20 Steel tube Area of brass rod (Ab) = Area of steel tube (A s) = x 202 314.16 mm2 4 x (362 302 ) 31102 . mm2 4 As E s 311.02 x 10 m x 210 x 10 N / m 2 0.653142 x 108 N 6 2 9 1 153106 . x 10 8 As E s Strength of Materials 36 Stress in steel tube = 5444.71N 17.51N / mm2 17.51 MN / m2 (Tension) 2 311.02 mm Stress in brass rod = 5444.71N 2 2 17 . 33 N / mm 17 . 33 MN / m (Compression) 2 314.16 mm (b) Stresses due to compression force, F’ of 20 kN F ' Es 20 x 103 N x 210 x 109 N / m2 2 s 46 . 44 MN / m (Compression) 8 E s As Eb Ab 0.653142 0.251327 x 10 F ' Eb 20 x 103 N x 80 x 109 N / m2 b 17.69 MN / m2 (Compression) 8 E s As Eb Ab 0.653142 0.251327 x 10 Resultant stress in steel tube = - 46.44 + 17.51 = 28.93 MN/m2 (Compression) Resultant stress in brass rod = -17.69 - 17.33 = 35.02 MN/m2 (Compression) Strength of Materials Example: 2 A railway is laid so that there is no stress in rail at 10º C. If rails are 30 m long Calculate, 1. The stress in rails at 60 º C if there is no allowance for expansion. 2. The stress in the rails at 60 º C if there is an expansion allowance of 10 mm per rail. 3. The expansion allowance if the stress in the rail is to be zero when temperature is 60 º C. 4. The maximum temp. to have no stress in the rails if the expansion allowance is 13 mm/rail.Take = 12 x Strength of Materials -6 10 per 1ºC E= 2 x 10 5 N/mm 2 Solution: 1. Rise in temp. = 60 º - 10 º = 50 ºC so stress = t E =12 x 10 -6 x50x 2 x 10 5 = 120 MPa 2. tp x L/E = = (L t -10) = (30000 x 12 x 10 -6 x50-10) = 18 -10 = 8 mm tp =E /L = 8x 2 x 10 5 /30000 = 53.3 MPa Strength of Materials 3. If stresses are zero , Expansion allowed =(L t ) = (30000 x 12 x 10 -6 x50) =18 mm 4. If stresses are zero tp =E /L*(L t -13)=0 L t=13 so t=13/ (30000 x 12 x 10 -6 )=360 C allowable temp.=10+36=460c. Strength of Materials Example: 3 A composite bar made up of aluminum and steel is held between two supports. The bars are stress free at 400c. What will be the stresses in the bars when the temp. drops to 200C, if (a) the supports are unyielding (b)the supports come nearer to each other by 0.1 mm. Take E al =0.7*105 N/mm2 ;al =23.4*10-6 /0C ES=2.1*105 N/mm2 s =11.7*10-6 /0C Aal=3 cm2 As=2 cm2 Strength of Materials Free contraction =Ls s t+ LALAlt Since contraction is checked tensile stresses will be set up. Force being same in both As s= Aal al contraction of steel bar s = (s/Es)*Ls contra.of aluminum bar al = (al/Eal)*Lal (a) When supports are unyielding s + al = (free contraction) (b) Supports are yielding s + al = ( - 0.1mm) Strength of Materials Example: 4 A steel bolt of length L passes through a copper tube of the same length, and the nut at the end is turned up just snug at room temp. Subsequently the nut is turned by 1/4 turn and the entire assembly is raised by temp 550C. Calculate the stress in bolt if L=500mm,pitch of nut is 2mm, area of copper tube =500sq.mm,area of steel bolt=400sq.mm • Es=2 * 105 N/mm2 ;s =12*10-6 /0C • Ec=1 * 105 N/mm2 ;c= 17.5*10-6 /0C Strength of Materials Solution: Two effects (i) tightening of nut (ii)raising temp. tensile stress in steel = compressive force in copper [Total extension of bolt +Total compression of tube] =Movement of Nut [s+ c] = np ( where p = pitch of nut) • PL/AsEs + s L t) +(PL/AcEc- c L t)=np Strength of Materials