ME 323 MIDTERM # 1: SOLUTION FALL SEMESTER Time allowed: 1hour

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Instructions ME 2 MIDTERM # : SOLUTION FALL SEMESTER 20 Time allowed: hour. Begin each problem in the space provided on the examination sheets. If additional space is required, use the yellow paper provided. Work on one side of each sheet only, with only one problem on a sheet. 2. Each problem is of equal value.. To obtain maximum credit for a problem, you must present your solution clearly. Accordingly: a. Identify coordinate systems b. Sketch free body diagrams c. State units explicitly d. Clarify your approach to the problem including assumptions 4. If your solution cannot be followed, it will be assumed that it is in error. 5. When handing in the test, make sure that ALL SHEETS are in the correct sequential order. Remove the staple and restaple, if necessary. Prob. Prob. 2 Prob. Total

Equations ε x = x E ε y = y E ε z = z E γ xy = τ G dφ γ = ρ dx dφ τ = Gρ dx [ σ ν ( σ + σ )] [ σ ν ( σ + σ )] [ σ ν ( σ + σ )] dφ dx xy γ xz y x x z z y = τ G 2 T G da = T = GI Tr τ = I p p TL ϕ = GI I I ε p crosssection dφ dx ρ p _ Circular _ Cross _ Section p _ Hollow_ Circular _ Cross _ Section L L = f i L i xz + αδt + αδt + αδt γ yz = τ G 4 π d = 2 π d d = 2 4 4 ( o i ) FL e= + LαΔT EA EA F = ( e LαΔT) L Failure Stress Yield Strength FS =, Allowable Stress State of Stress e = ucos( θ ) + vsin( θ ) yz 2

Problem In the structure shown below the Rod BD is made of aluminum ( σ Y = 60 x 0 ksi) with a cross-sectional area A BD = in 2. The pin at A is made of brass ( τ Y = 5 x 0 ksi), has a diameter d pin = 0.25 in and holds the structure in a single shear joint. Find the maximum force P max that can be applied at point C given that a Factor of Safety of 2.0 is required for both rod BD and pin A. Assume that bar ABC is rigid and that the diameter of pins B and C are large enough that they do not need to be considered. Only consider rod BD and the pin A in your calculation to find P max. A D m B m 4 m 4 m C P 5 4

Static equilibrium analysis to relate internal forces to P A y A A x y F BD m x B m C 4 m 4 m P 4 M A = 0 ( 4ft) FBD + ( 6ft) P ( 8ft) P = 0 5 5 F = 0 BD Fx = 0 Ax = P 5 4 4 Fy = 0 Ay = P FBD = P 5 5 Considering bar BD: σ failure 60 0 ksi σ allow = = = 0 0 ksi FS 2 2 F = σ A = 0 0 ksi in = 90 0 kips allow allow BD ( )( ) From static equilibrium analysis, F BD = 0, which means that F BD is independent of P and will never exceed Fallow for any value of P. F allow Considering Pin A: 4

τ allow τ failure 5 0 ksi = = = 7.5 0 ksi FS 2 π τ ( ) 4 2 2 Vallow = allowabd = 7.5 0 ksi 0.25 in = 86.5kips 2 Resultant force on pin: ( ) ( ) 2 F = A + A A x y Since this is a single shear pin, Vpin = FA Therefore, the maximum shear force on the pin is, V, = 86.5kips 2 2 4 V = 86.5kips = P + P 5 5 Pmax = 86.5kips = P allow, pin max max max allow pin 5

Problem 2 A mechanism for a thermal switch is shown below. The mechanism consists of two elastic bars of length L, elastic modulus E, coefficient of thermal expansion α, cross section area A. The mechanism is pinned to a rigid wall at B and D and at C the bar mechanism is pinned to a rigid roller. Both the bars are uniformly heated or cooled by the surrounding air temperature. Gravity is not to be considered in the problem. Assume a starting condition when the temperature is at and the gap is just closed, and the roller is just touching the wall (as shown), (a) Let the temperature be increased to a final temperature Tf so that T-T f c >0so the roller presses firmly against the wall. Using the method of sections draw a free body diagram. What additional equations do you need to solve for the internal axial forces? Derive an expression for the axial normal stress σ, σ2in the two rods in terms of α, LEA,, bar,( T f T c ). (b) Next let the temperature of the bars be decreased to a final temperature T f so that T-T f c < 0 and a gap opens up between the roller and the rigid wall. Using the method of sections draw a free body diagram and find the internal axial forces in the two bars. What is the axial normal stress σ, σ in the two rods? 2 T c D B 60 60 (2) 60 () C 6

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Problem The shaft AC is subjected to torsional loads at sections B and C. The diameters are d =50 mm and d 2 =20mm. (a) If the twist angle at point C is φ C =0.06rad determine the shear modulus (G) of the material of the shaft. (b) Determine the magnitude of the maximum shear stress in the shaft and indicate the location of maximum shear stress along the shaft, and location on the cross section. 8

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