PROBLEM #1.1 (4 + 4 points, no partial credit)

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σ = Eα(T T C PROBLEM #1.1 (4 + 4 points, no partial credit)

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PROBLEM #1.1 ( + points, no partial credit A thermal switch consists of a copper bar which under elevation of temperature closes a gap and closes an electrical circuit. The copper bar possesses a length L, modulus E, and coefficient of thermal epansion a. At room temperature T 0 the gap is d. (1 The gap is closed at a temperature T calculated from equation (circle one: (a d = α( T T 0 (b d = Lα ( T At T 0 (c d = Lα ( T T 0 (d d = Eα( T T 0 L d (2 As the temperature is increased beyond T, the there eist stress in the bar equal to (circle one: (a σ = Eα( T T 0 (b σ = Eα( T T (c σ = Eα( T T 0 (d σ = ELα( T T 0 1 ME 323 Final Eam, Sample & Solutions

PROBLEM #1.2 ( + points, no partial credit (1 A cylindrical pressure vessel with diameter D=2.5 m and wall thickness t=10 mm is filled with gas at an internal pressure of p=200 kpa. The absolute maimum shear stress in the vessel is (circle one (a 300 MPa (b 150 MPa (c 75 MPa (d 37.5 MPa (2 A propane tank with shape of a cylindrical pressure vessel has a diameter D=12 in. and a wall thickness of t=1/8 in. The tank is pressuried to p=200 psi. hoose the Mohr s circle diagram that corresponds to the state of stress (circle one. 2 ME 323 Final Eam, Sample & Solutions

PROBLEM #1.3 ( + points, no partial credit A circular torsion bar consists of a core material (diameter D core, shear modulus G core and a sleeve material (outer diameter D sleeve, G sleeve bonded firmly together at the interface. An eternal torque T is applied to the composite shaft. (1 In the analysis of this problem one needs to consider that (circle one: (a The stress distribution is possesses a jump (i.e. is discontinuous at the interface. (b The strain distribution is possesses a jump (i.e. is discontinuous at the interface. (c Both stress and strain possess a jump (i.e. are discontinuous at the interface. (d Neither stress and strain possess a jump (i.e. are discontinuous at the interface. (2 Which ones of the following statements are true regarding the maimum shear stress τ ma and its location in the bar? (circle one (a The maimum shear stress τ ma always occurs in the sleeve at the outer surface of the sleeve. (b If the cross sectional area of the sleeve is greater than that of the core, then the maimum stress τ ma occurs on the outer surface of the sleeve; and if the cross sectional area of the core is greater than that of the sleeve then τ ma occurs on the outer surface of the core. (c If GsleeveDsleeve > GcoreD then τ core ma occurs on the outer surface of the sleeve; and if GsleeveD sleeve <GcoreD then τ core ma occurs on the outer surface of the core. (d If GsleeveJsleeve > GcoreJ then τ core ma occurs on the outer surface of the sleeve; and if GsleeveJ sleeve <GcoreJ then τ core ma occurs on the outer surface of the core. (e The maimum shear stress τ ma always occurs at the outer surface of the core. (f None of the above. 3 ME 323 Final Eam, Sample & Solutions

PROBLEM #2 (25 points A truss structure consists of two members AB and B which are connected by pin joints. The rigid member AB is subjected to a distributed load of magnitude 10kN/m. The deformable member B possesses a circular cross section of diameter D. Determine the diameter of the truss B in order to prevent buckling of the member B with a factor of safety FS=2.9. onsider that the modulus of the material used for the truss B is E=210GPa. 10 kn/m 1 m 2 m ME 323 Final Eam, Sample & Solutions

5 ME 323 Final Eam, Sample & Solutions

PROBLEM #3 (25 points A Diameter d=1 cm Diameter D=3 cm 100 N A force is applied at point to a (very thin circular rigid plate with diameter D=3cm. The plate is attached to an elastic shaft (AB of diameter d=1cm and length L=10cm. All the strain energy is stored in the shaft (none in the plate since it is rigid. Also assume that strain energy stored due to transverse shear is negligible. The material is Aluminum (E= 73 GPa, G=27 GPa Using the work-energy principle determine the deflection of point in the direction of the applied force (i.e. along +y. Both torsion and bending are to be considered. B y 6 ME 323 Final Eam, Sample & Solutions

7 ME 323 Final Eam, Sample & Solutions

PROBLEM # (26 points At a particular cross section of a shaft the internal resultants were determined to consist of a torque (T = 2500 lb.in, a bending moment (M = 2000 lb.in and a shear force (V y = 300 lb. The shaft possesses a circular cross-section with radius r = 0.5 in. Determine the states of stress at locations A,B,,D on the cross-section. Document your answer by drawing the respective material elements at each location with the stress components clearly indicated by vectors and stress magnitudes. Determine the factor of safety using the vom Mises criterion, considering y that the yield strength is 30 ksi. A y V y = 300 lb B D T = 2500 lb.in 0.5 in M = 2000 lb.in 8 ME 323 Final Eam, Sample & Solutions

The stresses at points A, B,, and D will be due to torsion bending moment shear force A Torsion D T = T = 2500 lb.in y π 3 J = c = 98.17 10 in 2 Tc ( 2500 lb.in( 0.5 in τ = = = 12.73 ksi (W J 98.17 in ( B @ A, @ B, @, @ D, τ τ y = τ = 12.73 ksi (towards +Z = τ = 12.73 ksi (towards -Y τ = τ = 12.73 ksi (towards -Z τ y = τ = 12.73 ksi (towards +Y compressive A Bending moment M = 2000 lb.in π 3 I = c = 9.09 10 in M 2500 lb.in 0.5 in y + @A, σ = = I 9.09 10 3 in @B, @, @B, ( ( ( = 20.37 ksi (compressive M ( 2500 lb.in( 0 in y σ = = = 0 ksi I 9.09 10 3 in σ M y = = I ( ( 2500 lb.in( 0.5 in ( 9.09 10 3 in =+ 20.37 ksi (tensile M ( 2500 lb.in( 0 in y σ = = = 0 ksi I 9.09 10 3 in ( y B D tensile 9 ME 323 Final Eam, Sample & Solutions

Shear force A V = 300 lb y π 3 I = c = 9.09 10 in 3 @A &, Q = 0 in τ 0 ksi y=± 0.5 in y = y r π @B & D, Q = y 8.33 10 in y 0 in i Ai = r = = 3π 2 3 3 VQ ( 300 lb( 8.33 10 in y τ y = = 3 I t 9.09 10 in 2 0.5 in ' ' 2 3 3 ( ( = 0.51 ksi (downwards B D The combined state of stress at points A, B,, and D will be the resultant linear superposition of the individual stress values due to torsion, bending, and shear force. Point element A Point element B y Point element Point element D 10ME 323 Final Eam, Sample & Solutions

11ME 323 Final Eam, Sample & Solutions

12ME 323 Final Eam, Sample & Solutions