DEPARTMENT OF CIVIL ENGINEERING CE-221 SOLID MECHANICS End .

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DEPARTMENT OF CIVIL ENGINEERINGEnd-Sem ExamCE-221 SOLID MECHANICS16/11/15PAPER CODE: ANote: Write your name & roll no. on answerbook and on summary-answer-sheet provided with the question paper.You must submit the summary-answer-sheet along with the answerbook.Closed book, closed notes exam. No formula sheet allowed. No mobile phones allowed in the exam hall.All questions carry equal marks. Assume suitable data if required and state the same clearly.Use formulae from provided tables, if applicable.Problem 1The rectangular tube shown in Fig. 1 has a uniform wall thickness of 12 mm. For the givenloading, determine:(a) the normal stress acting on the cross section at points A and B.(b) the distance from A to the point where the neutral axis intersects line AB.Fig. 1Problem 2Two forces are applied to the pipe AB as shown in Fig. 2. The pipe has inner and outerdiameters of 35 mm and 42 mm respectively. Determine the maximum shearing stress(a) acting in the xy plane at point a,(b) acting in the zy plane at point b.Fig. 2

Problem 3The compound beam shown in Fig. 3 has fixed supports at A and D and consists of threemembers that are pinned together at B and C. Find the vertical deflection of the beam at thepoint where the load is applied.Fig. 3Problem 4Three uniform rigid bars of length a are interconnected by hinges at points 1 and 2 in therigid bar assemblage shown in Fig. 4. The lateral displacements of the assemblage areresisted by linear springs located at each hinge as shown in Fig. 4. The assemblage ishinged at point O and is guided to move vertically by rollers at point 3. Calculate thecritical load P of the assemblage when k1 k, k2 2k. Your answer should be in terms of aand k only.Fig. 4

Problem 5A cantilever beam carries a downward concentrated load of 10 kN at its free end. Thecomposite cross-section (see Fig. 5) comprises a 300mm x 100mm rectangular sectionhaving Youngs modulus E1 50 GPa which is bolted to a symmetric I-section havingYoungs modulus E2 200 GPa. The cross-sectional area and centroidal moment of inertia ofthe symmetric I-section are 2.02x104 mm2 and 7.475x108 mm4, respectively. The bolts areplaced two in a row (see Fig. 5) and spaced 600mm apart along the length of the beam.Determine:(a) The shear force carried by each bolt(b) The vertical shear stress in the rectangular section at the interface of the twomaterials.Fig. 5Problem 6A simply supported beam carrying a uniform load of 100 kN/m over its span of 10 m ismade of a solid rectangular section. The allowable normal stress of the beam is 150 MPa.The maximum deflection of the beam should not exceed 10 mm. Calculate the width anddepth of the cross-section such that the above mentioned capacities are fully utilized. E 200 GPa.

SUMMARY ANSWER SHEETPAPER CODE: AName:Roll no:Problem 1(a) A 31.52MPa B -10.39MPa(b) distance from A to point where neutral axis intersects line AB 94.01mmProblem 2(a) max shear stress in xy plane at a 17.58 GPa(b) max shear stress in zy plane at b 22.71 GPaProblem 3vertical deflection at point where load is applied 0.15625mProblem 4critical load P of assemblage 1 1 3 0.4226kaProblem 5(a) shear force carried by each bolt 3866N(b) vertical shear stress in rectangular section at interface 0.043MPaProblem 6width of cross-section 1.56mdepth of cross-section 0.02048m

DEPARTMENT OF CIVIL ENGINEERINGEnd-Sem ExamCE-221 SOLID MECHANICS16/11/15PAPER CODE: BNote: Write your name & roll no. on answerbook and on summary-answer-sheet provided with the question paper.You must submit the summary-answer-sheet along with the answerbook.Closed book, closed notes exam. No formula sheet allowed. No mobile phones allowed in the exam hall.All questions carry equal marks. Assume suitable data if required and state the same clearly.Use formulae from provided tables, if applicable.Problem 1The rectangular tube shown in Fig. 1 has a uniform wall thickness of 14 mm. For the givenloading, determine:(a) the normal stress acting on the cross section at points A and B.(b) the distance from A to the point where the neutral axis intersects line AB.Fig. 1Problem 2Two forces are applied to the pipe AB as shown in Fig. 2. The pipe has inner and outerdiameters of 32 mm and 38 mm respectively. Determine the maximum shearing stress(a) acting in the xy plane at point a,(b) acting in the zy plane at point b.Fig. 2

Problem 3The compound beam shown in Fig. 3 has fixed supports at A and D and consists of threemembers that are pinned together at B and C. Find the vertical deflection of the beam at thepoint where the load is applied.Fig. 3Problem 4Three uniform rigid bars of length a are interconnected by hinges at points 1 and 2 in therigid bar assemblage shown in Fig. 4. The lateral displacements of the assemblage areresisted by linear springs located at each hinge as shown in Fig. 4. The assemblage ishinged at point O and is guided to move vertically by rollers at point 3. Calculate thecritical load P of the assemblage when k1 2k, k2 3k. Your answer should be in terms ofa and k only.Fig. 4

Problem 5A cantilever beam carries a downward concentrated load of 12 kN at its free end. Thecomposite cross-section (see Fig. 5) comprises a 300mm x 150mm rectangular sectionhaving Youngs modulus E1 100 GPa which is bolted to a symmetric I-section havingYoungs modulus E2 200 GPa. The cross-sectional area and centroidal moment of inertia ofthe symmetric I-section are 2.02x104 mm2 and 7.475x108 mm4, respectively. The bolts areplaced two in a row (see Fig. 5) and spaced 800mm apart along the length of the beam.Determine:(a) The shear force carried by each bolt(b) The vertical shear stress in the rectangular section at the interface of the twomaterials.Fig. 5Problem 6A simply supported beam carrying a uniform load of 150 kN/m over its span of 15 m ismade of a solid rectangular section. The allowable normal stress of the beam is 175 MPa.The maximum deflection of the beam should not exceed 15 mm. Calculate the width anddepth of the cross-section such that the above mentioned capacities are fully utilized. E 250 GPa.

SUMMARY ANSWER SHEETPAPER CODE: BName:Roll no:Problem 1(a) A 23.04MPa B -6.99MPa(b) distance from A to point where neutral axis intersects line AB 115.07mmProblem 2(a) max shear stress in xy plane at a 29.83 GPa(b) max shear stress in zy plane at b 35.77 GPaProblem 3vertical deflection at point where load is applied 0.3125mProblem 4 5 7 0.7848kacritical load P of assemblage 3 Problem 5(a) shear force carried by each bolt 8810N(b) vertical shear stress in rectangular section at interface 0.073MPaProblem 6width of cross-section 2.1875mdepth of cross-section 0.03023m

DEPARTMENT OF CIVIL ENGINEERINGEnd-Sem ExamCE-221 SOLID MECHANICS16/11/15PAPER CODE: CNote: Write your name & roll no. on answerbook and on summary-answer-sheet provided with the question paper.You must submit the summary-answer-sheet along with the answerbook.Closed book, closed notes exam. No formula sheet allowed. No mobile phones allowed in the exam hall.All questions carry equal marks. Assume suitable data if required and state the same clearly.Use formulae from provided tables, if applicable.Problem 1The rectangular tube shown in Fig. 1 has a uniform wall thickness of 10 mm. For the givenloading, determine:(a) the normal stress acting on the cross section at points A and B.(b) the distance from A to the point where the neutral axis intersects line AB.Fig. 1Problem 2Two forces are applied to the pipe AB as shown in Fig. 2. The pipe has inner and outerdiameters of 42 mm and 48 mm respectively. Determine the maximum shearing stress(a) acting in the xy plane at point a,(b) acting in the zy plane at point b.Fig. 2

Problem 3The compound beam shown in Fig. 3 has fixed supports at A and D and consists of threemembers that are pinned together at B and C. Find the vertical deflection of the beam at thepoint where the load is applied.Fig. 3Problem 4Three uniform rigid bars of length a are interconnected by hinges at points 1 and 2 in therigid bar assemblage shown in Fig. 4. The lateral displacements of the assemblage areresisted by linear springs located at each hinge as shown in Fig. 4. The assemblage ishinged at point O and is guided to move vertically by rollers at point 3. Calculate thecritical load P of the assemblage when k1 3k, k2 4k. Your answer should be in terms ofa and k only.Fig. 4

Problem 5A cantilever beam carries a downward concentrated load of 18 kN at its free end. Thecomposite cross-section (see Fig. 5) comprises a 300mm x 200mm rectangular sectionhaving Youngs modulus E1 75 GPa which is bolted to a symmetric I-section havingYoungs modulus E2 200 GPa. The cross-sectional area and centroidal moment of inertia ofthe symmetric I-section are 2.02x104 mm2 and 7.475x108 mm4, respectively. The bolts areplaced two in a row (see Fig. 5) and spaced 1000mm apart along the length of the beam.Determine:(a) The shear force carried by each bolt(b) The vertical shear stress in the rectangular section at the interface of the twomaterials.Fig. 5Problem 6A simply supported beam carrying a uniform load of 200 kN/m over its span of 20 m ismade of a solid rectangular section. The allowable normal stress of the beam is 200 MPa.The maximum deflection of the beam should not exceed 40 mm. Calculate the width anddepth of the cross-section such that the above mentioned capacities are fully utilized. E 150 GPa.

SUMMARY ANSWER SHEETPAPER CODE: CName:Roll no:Problem 1(a) A 47.96MPa B -17.86MPa(b) distance from A to point where neutral axis intersects line AB 72.87mmProblem 2(a) max shear stress in xy plane at a 23.44 GPa(b) max shear stress in zy plane at b 28.63 GPaProblem 3vertical deflection at point where load is applied 0.46875mProblem 4 7 13 1.1315kacritical load P of assemblage 3 Problem 5(a) shear force carried by each bolt 15768N(b) vertical shear stress in rectangular section at interface 0.105MPaProblem 6width of cross-section 2.778mdepth of cross-section 0.03888m

DEPARTMENT OF CIVIL ENGINEERINGEnd-Sem ExamCE-221 SOLID MECHANICS16/11/15PAPER CODE: DNote: Write your name & roll no. on answerbook and on summary-answer-sheet provided with the question paper.You must submit the summary-answer-sheet along with the answerbook.Closed book, closed notes exam. No formula sheet allowed. No mobile phones allowed in the exam hall.All questions carry equal marks. Assume suitable data if required and state the same clearly.Use formulae from provided tables, if applicable.Problem 1The rectangular tube shown in Fig. 1 has a uniform wall thickness of 8 mm. For the givenloading, determine:(a) the normal stress acting on the cross section at points A and B.(b) the distance from A to the point where the neutral axis intersects line AB.Fig. 1Problem 2Two forces are applied to the pipe AB as shown in Fig. 2. The pipe has inner and outerdiameters of 28 mm and 32 mm respectively. Determine the maximum shearing stress(a) acting in the xy plane at point a,(b) acting in the zy plane at point b.Fig. 2

Problem 3The compound beam shown in Fig. 3 has fixed supports at A and D and consists of threemembers that are pinned together at B and C. Find the vertical deflection of the beam at thepoint where the load is applied.Fig. 3Problem 4Three uniform rigid bars of length a are interconnected by hinges at points 1 and 2 in therigid bar assemblage shown in Fig. 4. The lateral displacements of the assemblage areresisted by linear springs located at each hinge as shown in Fig. 4. The assemblage ishinged at point O and is guided to move vertically by rollers at point 3. Calculate thecritical load P of the assemblage when k1 4k, k2 5k. Your answer should be in terms ofa and k only.Fig. 4

Problem 5A cantilever beam carries a downward concentrated load of 30 kN at its free end. Thecomposite cross-section (see Fig. 5) comprises a 300mm x 250mm rectangular sectionhaving Youngs modulus E1 50 GPa which is bolted to a symmetric I-section havingYoungs modulus E2 400 GPa. The cross-sectional area and centroidal moment of inertia ofthe symmetric I-section are 2.02x104 mm2 and 7.475x108 mm4, respectively. The bolts areplaced two in a row (see Fig. 5) and spaced 1200mm apart along the length of the beam.Determine:(a) The shear force carried by each bolt(b) The vertical shear stress in the rectangular section at the interface of the twomaterials.Fig. 5Problem 6A simply supported beam carrying a uniform load of 120 kN/m over its span of 5 m ismade of a solid rectangular section. The allowable normal stress of the beam is 250 MPa.The maximum deflection of the beam should not exceed 5 mm. Calculate the width anddepth of the cross-section such that the above mentioned capacities are fully utilized. E 300 GPa.

SUMMARY ANSWER SHEETPAPER CODE: DName:Roll no:Problem 1(a) A 60.66MPa B -20.66MPa(b) distance from A to point where neutral axis intersects line AB 55.94mmProblem 2(a) max shear stress in xy plane at a 45.08 GPa(b) max shear stress in zy plane at b 55.90 GPaProblem 3vertical deflection at point where load is applied 0.625mProblem 4 9 21 1.4725kacritical load P of assemblage 3 Problem 5(a) shear force carried by each bolt 25319N(b) vertical shear stress in rectangular section at interface 0.141MPaProblem 6width of cross-section 0.8681mdepth of cross-section 0.01194m

DEPARTMENT OF CIVIL ENGINEERING CE-221 SOLID MECHANICS End-Sem Exam 16/11/15 PAPER CODE: C Note: Write your name & roll no. on answerbook and on summary-answer-sheet provided with the question paper. You must submit the summary-answer-sheet along with the answerbook. Closed book, closed notes exam.

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