MAKE 2 COPIES OF COVER PAGE PHYSICS 23 LABORATORY E6-SHEAR MODULUS NAME: Partner’s Name: Laboratory Instructor: Laboratory Section: Recitation Instructor: Recitation Section: OBJECTIVES: To determine the shear modulus of a rod. Key Words: Reading: Introduction: In this experiment we wish to get a feeling for what happens to a “rigid” body when we apply forces to it. These forces (and torques) sum to zero so that the body remains in static equilibrium after the forces are applied. This is a problem of fundamental concern to many engineers. Will the bridge collapse when a heavy truck is driven over it? Will the engine break loose from the wing during takeoff? Will the roof of the arena fall under heavy wind and water loads? As good scientists and engineers, we shall begin by trying very simple approximations and testing them against our measurements in the laboratory to see if they are sufficient. We know that rigid bodies are not really rigid. They distort under applied forces. Our simple assumption will be that they distort like springs. That is, if we pull on a rod, the change in length is proportional to how hard we pull. In other words, we expect a behavior like F = -kx for a spring (remember x in this equation is the change in length of the spring). Suppose we pull on a rod of length L0 with a force F as shown. We would like our results to be good for all rods of length L0 whether 1 inch in diameter or ten feet. Define the stress, S, by F . A A is the cross sectional area of the rod. In this particular case, we have tensile stress S= because we are stretching the rod. Note the units of stress are newtons / m 2 or dynes / cm 2 . The rod responds to our applied force by stretching an amount L. We wish to have our results not dependent upon the original length of the rod, L0 so we define the strain by the ratio of increase in length to the original length: L Tensile strain = L0 Now we make our assumption that the bar behaves like a spring, namely, Stress = Y * Strain Or F A Y LL0 L0 L F F L0 + L Y is the constant of proportionality called Young’s modulus or the stretch modulus. Note that it does not depend upon the length of the rod or its cross sectional area. It is a property of the material of which the rod is made. Since the strain is a pure number (just the ratio of two lengths), Young’s modulus has the same dimensions as stress. Let’s see how big an effect this is: Just how non-rigid is an aluminum rod. Being naturally lazy, let’s take a rod one meter long and 1 cm in diameter. Thus A = πd 2 /4 = π/4 cm 2 . Tables of Young’s modulus give for aluminum. YAl = 0.70 X 10 12 dynes/cm 2 . Suppose we suspend the rod vertically and hang a 10 kg weight on it and want to measure the change in length of the rod. The gravitational force on a 10kg weight is F = mg = 10 X 10 3 gm X 980 cm/sec 2 = 9.8 X 10 6 dynes. Hence L L0 F AY 9.8*106 12 4 *0.7*10 178 . *105 meters Or the rod stretches L= 1.78 * 10 5 * 100 cm = 1.75 X 10 3 cm. Previous experiments should have convinced you that you do not want to measure a 0.002 cm change in length in a meter rod using the equipment available in this laboratory! Note that eq. (l) can be written F YA L0 L So if we put k = YA / L0 and write the changes in length, L, as x, we have Hook’s law F = kx. Since F here is the force we apply, this becomes F=-kx if F is the force the rod exerts on us. Since it appears difficult to measure L with our experiment, let’s consider the rotational equivalent of the above experiment. F The rod shown is clamped on the left hand side so that the left hand end cannot rotate. The right hand end is supported by bearings so it can rotate but not translate. None of this is shown in the drawing. Note that when we apply F and hence a torque, = rF, the rod twists through an angle. That little arrow on the end of the rod is supposed to be a pointer so we can measure the angle . For rotation, recall that F and x, so Hooke’s law, F = -kx, becomes = - k’ for rotation. Once again, we would like to assume that our rod behaves like a spring obeying this Hooke’s law for rotational “stretching.” This analysis is more complicated than for the linear stretching case, but once again the basic assumption is that shearing stress is proportional to shearing strain, and the constant of proportionality, E, is called the shear modulus: shearing stress = E * (shearing strain) The shearing strain is just the angular rotation per meter of rod: shearing strain L0 One finds eventually that 2 L0 E r 4 In our experiment, we apply F, not at the radius of the rod, r, but at a larger radius, R, so = FR. The shearing stress is proportional to the torque so that eq. (2) can be written = - k’ , (where is the torque the rod exerts against us) since the shearing strain is proportional to . Note that this is just the rotational analog of F =-kx. Apparatus: Torsion lathe and specimens; Vernier caliper; weight pan and weights Procedure: 1. Measure the dimensions of the specimen and place it in the torsion lathe, setting the Vernier to zero with the weight pan in place. 2. Add loads to the pan up to the maximum load which will produce a twist of no more than about 60 degrees (you need only use four masses ranging up to 500 gms). Record the angle of twist both for the loading, load, and the unloading process, unload. To help minimize friction effects use 1 the average value of avg = ( load + unload). 2 3. Take the necessary measurements to enable you to convert load to torque. Remember torque = = RF = Rmg where R is the radius of the large wheel. 4. Repeat steps 1-3 with a second specimen. Measurements: Analysis: 1. Make a table of torque in Newton-meters vs angle in rad. Plot a graph of torque in Newton-meters vs angle in radians. From the slope of this graph, determine E and compare this result with accepted values. Hint: Use eq. (3) to find the relation between the slope of vs. and the constant E. Compute the percent deviation between your measured value and the handbook value for the same material. 2. Repeat for the second specimen. Conclusions: Material Shear Modulus Aluminum Brass Copper Iron Lead Magnesium Molybdenum Nickel Steel Tungsten 1010 N m 2.37 3.53 4.24 7.0 0.54 1.67 14.7 7.06-7.55 7.79 14.81 2 From CRC Handbook of Chemistry and Physics