Size: px
Start display at page:

Download ""

Transcription

1 (SO/EC Certified) Model nswer: Summer 7 Code: 17 mportant nstrutions to examiners: 1) The answers should e examined y key words and not as word-to-word as given in the model answer sheme. ) The model answer and the answer written y andidate may vary ut the examiner may try to assess the understanding level of the andidate. ) The language errors suh as grammatial, spelling errors should not e given more importane. (Not appliale for sujet English and Communiation Skills.) ) While assessing figures, examiner may give redit for prinipal omponents indiated in the figure. The figures drawn y the andidate and those in the model answer may vary. The examiner may give redit for any equivalent figure drawn. 5) Credits may e given step wise for numerial prolems. n some ases, the assumed onstant values may vary and there may e some differene in the andidate s answers and the model answer. 6) n ase of some questions redit may e given y judgment on part of examiner of relevant answer ased on andidate s understanding. 7) For programming language papers, redit may e given to any other program ased on equivalent onept Q 1 a) ttempt any SX of the following: 1 i) Define elastiity and modulus of elastiity. Elastiity: - Elastiity is the property of material y virtue of it an regain its original shape and size after removal of deforming fore. 0 Modulus of Elastiity: - t is defined as the ratio of stress to strain within elasti limit. ii) Define angle of oliquity. ngle of Oliquity : - The angle that the line of ation of the resultant stress makes with the normal to the plane is alled the angle of oliquity 0 0 iii) State the parallel axis theorem. t states that the M.. of a plane setion aout any axis parallel to the entroidal axis is equal to the M.. of the setion aout the entroidal axis plus the produt of the area of the setion and the square of the distane etween the two axes. 0 0 age 1 /

2 (SO/EC Certified) Model nswer: Summer 7 Code: 17 1 = G +h iv) What do you mean y eentri load? Show y simple sketh eentrially applied load. Eentri load: - The load whose line of ation does not oinide with the axis of the memer is alled as eentri load. 0 v) State any four assumptions made in the theory of pure torsion. ssumptions in the Theory of ure Torsion. 1. The material of the shaft is homogenous and isotropi and follows Hook s law.. The twist along the shaft is uniform.. The shaft is straight and having uniform irular ross setion throughout.. Cross setions of the shaft whih are plane efore twist remain plane after twist. 5. Stresses do not exeed the proportional limit. ½ mark eah (ny four) 0 age /

3 (SO/EC Certified) Model nswer: Summer 7 Code: 17 1 vi) Define ulk modulus. ulk Modulus: - When a ody is sujeted to three mutually perpendiular like stresses of same intensity then the ratio of diret stress to the orresponding volumetri strain of the ody is onstant and is alled as ulk modulus. 0 0 vii) Define hoop stress. State the formula. Hoop stress the stress whih at in the tangential diretion to the irumferene of the ylinder alled as hoop stress or irumfertial stress Hoop Stress, d t Where, Hoop stress Or Cirumferential stress nternal liquid pressure d = nternal daimeter of thin ylinder t = Thikness 0 viii) State middle third rule. n retangular setion for no tension ondition the load must lie within the middle third shaded area of size and d. This is known as 0 0 middle third rule. age /

4 (SO/EC Certified) Model nswer: Summer 7 Code: 17 Q. 1 ) ttempt any Two of the following: 08 i) metal rod mm diameter and meter long is sujeted to an axial pull of 0 kn. f the elongation of the rod is 0.5mm, find the stress indued and the value of Young s modulus. Given: rea, Stress ( ), d mm, L m 0kN 0 N l 0.5mm? E? d () 5.89mm N mm Young ' s mod ulus( E) E E L l E N / mm ii) simply supported eam of span 9.75m is arrying full span u.d.l. of 10 kn/m. What is the magnitude and position of maximum ending moment developed? To find the support reation, R Fy 0 R ( ) 0 R R 97.5 KN... 1 age /

5 (SO/EC Certified) Model nswer: Summer 7 Code: 17 1 Taking moment at, R R R M R R ut R in R R R KN 97.5 eq n R 8.75KN SF alulation, SF. 0 L SF R SF L SF L SF. 0 R s S. F. is zero at pt. C To find pt of ontra shear SF. 0 C SF C m MD 1 Mark. M Calulation, M. 0 M M. C M kn m C. M at C is the max. M. as at C S. F. is zero age 5 /

6 (SO/EC Certified) Model nswer: Summer 7 Code: 17 1 iii) irular eam of 10mm diameter is simply supported over a span of 10m and arries u.d.l of 1000 N/m. find the maximum ending stress produed. Given data : d 10 mm, L 10m 10000mm w 1000 N m 1000 w N mm 1N mm 1000? Max. ending Moment, M wl M M N mm Moment of nertia, 6 6 d mm d 10 y 60mm y y y 60mm Max. ending stress, M y t N mm ttempt any FOUR of the following: 16 a) i) What is meant y modular ratio? ii) State any four assumptions made in Euler s theory. i) Modular Ratio: The ratio of modulus of elastiity of two different materials is alled as modular ratio. t is denoted y m. 0 m E E 1 E 1 >E age 6 /

7 (SO/EC Certified) Model nswer: Summer 7 Code: 17 Following are the assumptions in the Euler s theory. a) The material of the olumn is perfetly homogenous and isotropi. ) The olumn is initially perfetly straight and is axially loaded. ) The ross setion of the olumn is uniform. d) The length of olumn is very large ompared to the lateral ½ marks eah (any four) dimensions. e) The self-weight of olumn is negleted. f) The olumn will fail y ukling only. ) irular steel ar of 10 mm diameter and 1.m long is sujeted to a ompressive load in testing mahine. ssuming oth ends hinged, alulate Euler s rippling load. lso alulate safe load y onsidering fator of safety as. Take E=x10 5 N/mm. Given data : d 10 mm, L 1.m 100 mm, fos, E 10 N / mm r? safe load? 5 For olumn with oth ends hinged Le l 100mm M.. for irular se tion, d 6 (10) mm Eulers rippling load, r r E Le (100) r N age 7 /

8 (SO/EC Certified) Model nswer: Summer 7 Code: 17 rippling load Safe load F. O. S Safe load Safe load.9n ) steel ue lok of 50mm side is sujeted to a fore of 6 kn (tensile) along X-diretion; 8 kn. (ompressive) along Y diretion and kn (tensile) along Z diretion. Determine hange in the 10 volume of the lok. Take E=00 Ga and m. Given data : l t 50mm x 6kN 6000 N ( Tensile) y 8kN 8000 N ( omprtessive) z kn 000 N ( Tensile) E 00Gpa 00 N / mm 10 m, 0. Find : v? Stress along x diretion x 6000 x. N / mm 5050 Stress along y diretion y 8000 y 5050 Stress along z diretion z N / mm z z. N / mm ( ompressive) original volume ( V ) V Lt V V 1510 mm age 8 /

9 (SO/EC Certified) Model nswer: Summer 7 Code: 17 For triaxial stress system x y z ev (1 ) E v x y z (1 ) V E v (1 0.) v v v 0.mm Change in volume is 0.mm d) onrete olumn 00mm X 00mm is reinfored with ars of 0mm diameter and arries a ompressive load of 00kN. The modular ratio is 15. Calulate the stresses in steel and onrete. lso alulate the load shared y eah material. Given data : rea of onrete olumn, 0000mm Diameter of steel ar, d 0mm of steel ar, n Load, p 00kN 00 N m 15???? s s rea of steel ar( ) s n d s 0 s s mm age 9 /

10 (SO/EC Certified) Model nswer: Summer 7 Code: 17 rea of onrete ( ), mm s as, m s 15 s also, ut, s s s ( ) (887.6 ) 00 ( ) s N / mm s, 15 s s N / mm s Load shared steel s s s s s N s kN ½ Load shared y eonrete N 9.859kN ½ age 10 /

11 (SO/EC Certified) Model nswer: Summer 7 Code: 17 e) antilever eam of length 10m arries two points load of magnitude 0kN and 0 kn at m and free end respetively. Draw the S.F.D and.m.d. Re ation at fixed end R R kN S. F. alulation SF.. 0 L S. F. 50 kn R S. F. 50 kn L S. F kn R S. F kn CL SF CR M alulation, M.. 0 C M M. 180 kn m M 0 0. M. 80 kn m age 11 /

12 (SO/EC Certified) Model nswer: Summer 7 Code: 17 OR S. F. alulation SF.. 0 L S. F. 50 kn R S. F. 50 kn L S. F kn R S. F kn CL SF CR M alulation, M.. 0 C M.. 0. M. 10 kn m M M. 0 kn m f) gas ylinder of internal diameter 1.m and thikness mm is sujeted to a maximum tensile stress of 90 Ma. Find the allowale pressure of gas inside ylinder. age 1 /

13 (SO/EC Certified) Model nswer: Summer 7 Code: 17 nternal daimeter d = 1. m = 100mm Thikness, t = mm Tensile stress, 90Ma 90 N / mm r essure of gas, p =? s tensile stress = Hoop Stress = 90 N / mm d. t N / mm 0 0 ttempt any FOUR of the following: 16 a) Draw S.F. and.m. diagram for simply supported eam of span L arrying a entral point load W. State the value of maximum shear fore and maximum ending moment. W Max. S. F = Max..M= WL age 1 /

14 (SO/EC Certified) Model nswer: Summer 7 Code: 17 ) Define point of ontra flexure. How is the point of ontra flexure loated for a eam? oint of ontra-flexure: - The point at whih ending moment diagram hanges the sign from positive to negative or vie versa or the point at whih M is zero is alled as point of ontra-flexure 0 Loation of point of ontra-flexure i) t the point of ontra-flexure.m is zero. ii) Take.M at the point of ontra-flexure and equate with zero. iii) The distane (loation) of point of ontra-flexure will e find from either end of eam. oint D,.M. = 0 oint D is oint of Contraflexure. oint D is at Z m from ) simply supported eam of m span arries two point loads of 5 kn eah at 1 m and m from the left end. Draw the shear fore and ending moment diagram. age 1 /

15 (SO/EC Certified) Model nswer: Summer 7 Code: 17 Step i) To find support reations, Sine loading is symmetial R R 5 kn Step ii) SF alulations SF.. 5 kn SF.. 5 kn L SF = 0 kn R SF.. = 0 kn C L SF.. = -5 kn C R SF.. = -5 kn D L D SF.. = 0 kn D Step iii) M.. Calulation, Sine the supports are simple.m. 0.M. 0 D M kn-m M kn-m C ½ ½ age 15 /

16 (SO/EC Certified) Model nswer: Summer 7 Code: 17 d) eam 6 m long rests on two supports 5 m apart. The right end is overhang y 1 m. the eam arries a u.d.l. of 5 kn/m over the entire length of the eam. Draw S.F. and. M. diagram. To find support reations, F 0 Y R 56 R 0 R R 0...(i) Taking moment at 6 R R 5 0 R 5 90 R 18 kn ut R in equation (i) R R 0 R 18 0 R 1 kn S. F. Calulation, SF.. = 0 L S. F. 1 kn R L R C L C R SF = -1 kn SF = 5 kn SF.. = = 0 SF.. = 0 Shear fore is zero at pt. D and the pt. D is at 'x' m from SF.. = 0 D SF.. = 1 5 x 0 D 5 x 1 x =. m M.. Calulation,.M. 0..M. D M. 5 kn m D SF al. SFD and MD (1 mark eah) M al. age 16 /

17 (SO/EC Certified) Model nswer: Summer 7 Code: 17 M.. 1. kn-m D 5 M M. = -.5 kn m M.. 0 C M.. is zero at pt. E t. E is at Y m from Y. M. E 1Y -5 Y = 0 Y Y = 0 Y =.8 m from e) point in a strained material stresses are sujeted to two mutually perpendiular tensile stresses of 00 Mpa and 100 Mpa. Determine the intensities of normal, shear a resultant stresses on a plane inlined at 0 0 with the axis of minor tensile stress. Given data: 00 Ma, 00Ma x ) nalytial Method??? n t R x y x y n os sin n os 0 0 x n 15 N/mm x y t sin os t sin 0 0. N/mm t age 17 /

18 (SO/EC Certified) Model nswer: Summer 7 Code: 17 Resultant Stress, R R n t (15) (.) R 1.87 N / mm OR ) Mohr s Cirle method (Graphial) f) Find the M.. of a T setion having top flange 00 mm 0 mm and we 00 mm 0 mm aout the entroidal axis X-X and Y-Y. Given data : 0 mm, d 00mm mm, d 0mm d mm d mm as the T se tion is symmetrial aout y axis 00 X 100 mm To find Y y d mm 1 1 age 18 /

19 (SO/EC Certified) Model nswer: Summer 7 Code: 17 y 1 d mm ( Y 1 1) ( Y ) Y (0000) (000 10) Y ( ) Y 155mm To find M.. aout X X xx x 1 x 1 x d x a 1 1h1 1 h mm (000 ) 1 ( ) x mm 6 x x x d ah 1 h mm (000 ) mm XX X1 X XX YY ( ) 6 = mm Y1 Y To find M.. at Y-Y axis d11 d YY a1h1 ah 1 1 h h 0 as symmetrial at Y axis 1 YY YY mm 6 age 19 /

20 (SO/EC Certified) Model nswer: Summer 7 Code: 17 Q. ttempt any FOUR of the following: 16 a) Find the moment of inertia of a square of side a aout its outer edge. i) For a square of side 'a' a. a a xx 1 1 ii) rea of setion, = a a a iii) The outer edge is paralle to XX axis Distane etween XX axis and Outer edge is a h = iv) Using the parallel axis theorom, M.. aout parallel axis = M.. aout entroidal axis + h h xx a a = a 1 a a 1 a 0 ) hannel setion 100m 100m 0m thik. Find the moment of inertia aout entroidal axis X-X and Y-Y. X a x a x a x a a a (100000) 500 (100000) 500 (0000) 150 (100000) (100000) (0000) X 1.667mm XX D d 1 1 age 0 /

21 (SO/EC Certified) Model nswer: Summer 7 Code: 17 XX XX 1 = mm YY Y1 Y1 YY YY 1 Y 1Y 1 YY d h 1 1 Y = Y 1 YY mm Y1 Y1 YY 10 1 YY d h 1 1 = mm YY YY mm ) n isoseles triangular setion C has ase width 80 mm and height 60 mm. Determine the M.. of the setion aout the C. G. of the setion and the ase C. ase ase xx xx h mm h mm d) hole of 100 mm diameter ut from a retangular plate 600 mm wide and 00 mm deep. The enter of hole is at 160 mm from the edge on an axis iseting shorter side. Find M.. of remaining plate aout X-X and Y-Y axis. X a1x1 ax a1 a (600 00) 100 (600 00) X.76mm age 1 /

22 (SO/EC Certified) Model nswer: Summer 7 Code: 17 XX XX XX D d (100) mm D YY h d h 1 6 YY (100) (100) YY mm State any four assumptions made in the theory of simple ending. e) ssumptions 1. The material of the eam is homogeneous and isotropi and follows the Hooke's Law.. The transverse setion of the eam whih is plane efore ending will remain plane after ending.. Young's modulus for the material is same for tension and ompression 1 mark eah (any four). Eah layer is free to expand or ontrat independently. 5. The eam in initially straight and of onstant ross setion. age /

23 (SO/EC Certified) Model nswer: Summer 7 Code: 17 f) eam 100mm wide and 50mm deep is sujeted to a shear fore of 0KN at a ertain setion find the maximum shear stress and draw the shear stress variation diagram. q q av max S S 0 d 500 q av max 1.6 N / mm 1.5 q q av. N / mm age /

24 (SO/EC Certified) Model nswer: Summer 7 Code: 17 5 ttempt any FOUR of the following: 16 a) timer eam has a ross setion 10 mm X 00 mm. t is simply supported over a span of m and arries a u.d.l. of 1 kn/m over the entire span. Calulate the maximum ending stress indued in eam and the radius of urvature to whih the eam will end at the setion. M E y R wl M 10 N mm ½ d mm 1 1 d 00 Y 100 mm 6 M 10 Y N / mm 80 M E OR y y R E E R OR R Y M E E R 6 OR R ½ R 0E OR R 0E Note: - f suitale value of E is assume should e onsider ) irular setion of diameter d is sujeted to load eentri to the axis the eentriity of load is e otain the limit of eentriity suh that no tension is indued at the setion. To find : e=? Diret stress, σ= 0 ending stress, M σ= Z age /

25 (SO/EC Certified) Model nswer: Summer 7 Code: 17 5 for irular se tion, d 6 d y d Z 6 d y d for no tension ondition, 0 M Z e Z 1 e Z d Z e d d e 8 The ore of a setion is d d irle of radius e = or diameter 8 ) retangular olumn 150mm wide and 100mm thik arries a load of 150 kn at an eentriity of 50mm in the plane iseting the thikness. Find the maximum and minimum intensities of stress. lso draw stress distriution diagram. Given data: = 150 mm, d = 100mm = 150 kn, e = 50mm σ =? σ =? max min rea of setion, = d= =15 10 mm age 5 /

26 (SO/EC Certified) Model nswer: Summer 7 Code: 17 5 Diret stress, σ= σ= σ 0 =10 N mm (C) ½ ending Stress, M σ= Z yy e σ= d 6 6e σ= d Diag. ½ σ= 1050 σ = 0 N mm σ = σ + σ = σ max 0 max = 0 N mm (C) 0 ½ σ = σ - σ = 10-0 σ min 0 min = 10 N mm (T) ½ d) square olumn 00mm X 00 mm arries an axial load of 00 kn. Find the position of 0 kn load ating along the axis iseting the width of the ross setion so that the stress developed at the other extreme of the olumn will e zero N / mm M Y 150 mm mm 1 1 e age 6 /

27 (SO/EC Certified) Model nswer: Summer 7 Code: 17 5 M Y 0 0 e For no tension ondition, e 8.5mm e e 0 e) square pillar is 600mm X 600mm in setion. t what eentriity a point load of 6000 kn is plaed on one of the entroidal axis of the setion so as to produe no tension in the setion. For no tension ondition, 0 M Z.. ey e Y e 100mm f) mild steel flat 50mm wide and 5mm thik is sujeted to load ating in the plane iseting the thikness at a point 10mm away of the entroid of the setion. f the tensile stress is not to exeed 150 Ma, alulate the magnitude of. Given data : 50 mm, d 5 mm, e 10 mm, max? 150Ma 150 N mm ( tensile) d mm age 7 /

28 (SO/EC Certified) Model nswer: Summer 7 Code: M e 6 e Z d 6 d yy max N kN 6 ttempt any FOUR of the following: 16 a) hollow shaft is of the same external diameter as that of the solid shaft. The inside diameter of the hollow shaft eing half the external diameter. oth the shafts have the same material and length. Then show that the ratio of torque transmitted y hollow shaft to the torque transmitted y solid shaft is T Gθ = J L G.θ T Hollow = J L G.θ T Solid = JSolid L G.θ J T Hollow L = T Solid G.θ J L THollow JHollow = T J Solid Solid Hollow Hollow Solid ut, π J Hollow = D -d π D J Hollow = D - age 8 /

29 (SO/EC Certified) Model nswer: Summer 7 Code: 17 6 π J Solid = D π D D- T Hollow = T π Solid D 16D -D = 16D T T Hollow Solid =0.975 ) shaft is transmitting 150 kw at 00 RM. f allowale shear stress is 80N/mm and allowale twist is per m, find the diameter of shaft. Take C = 0.8 X 10 5 N/mm ower =150 kw= W Speed N=00rpm Shear stress f =80N/mm 1.5 π 0 θ=1.5 = rad 180 Length L= m=000mm S C= N/mm 5 Find Case i) mean D=? πnt = watts 60 π 00 T = 60 T = N.m mean T = N.mm mean Case ii) Diameter ased on shear stress: T mean = T max Using relation, π T max= f S D 16 π = 80 D 16 D = mm age 9 /

30 (SO/EC Certified) Model nswer: Summer 7 Code: 17 6 max = 180 π 000 Case iii) Diameter ased on angle of twist Using relation, T Cθ = L D D=108.6 mm π Note: - dopt higher value of Diameter i.e mm eause it will satisfy oth shear stress and angle of twist. ) Calulate the suitale diameter of the solid shaft to transmit 0 kw at 150 rpm if the permissile shear stress is 68 Ma. Given data: ower = 0 kw = 0 10 W Speed N = 150 rpm Shear stress, f = 68 Ma = 68 N/mm S find : D i) Using the relation, = 0 10 = πnt watts 60 π 150 T 60 T = N.m T = ii)using the relation, 10 N -mm π T= f S D 16 π = 68 D 16 D = 1.6 mm age 0 /

31 (SO/EC Certified) Model nswer: Summer 7 Code: 17 6 d) Selet a suitale diameter for a solid shaft to transmit 00 H at 180 rpm. The allowale shear stress is 80 N/mm. Given data: ower =00H Speed N=180rpm Shear stress f =80N/mm π 0 θ=1 = rad 180 Length L=m=000mm S C= N/mm 5 Find D=? f the power is given in terms of H then πnt = H 500 π 180 T 00= 500 T=795.77kg.m T= = N.m T= N.mm Diameter ased on shear stress Using relation, π T= f S D 16 π = 80 D 16 D=79.1 mm Note: - f suitale value modulus of rigidity assumed to alulate diameter of solid shaft should e onsider. age 1 /

32 (SO/EC Certified) Model nswer: Summer 7 Code: 17 6 e) hollow shaft is of external diameter and internal diameter 00mm and 00mm respetively. Find the maximum torque is an transmit, if the angle of twist is not to exeed in a length of 10m. take C = 0.8X10 5 N/mm Given data: External diameter, D = 00mm nternal diameter, d=00mm 0 θ =1.5 =1.5 = 0.06 rad Length L=10m=10 10 mm π 180 C= N/mm Find T=? 5 y using torsional relation T Cθ = L Cθ π Cθ T = = (D - d ) L L 5 π T = (00-00 ) π 10 T = T = N.mm T = 9.8 kn.m f) (i) Differene etween pure ending and ordinary ending (ii) Write the equation of torque transmitted y the O.C. shaft giving meaning and unit of eah term. age /

33 (SO/EC Certified) Model nswer: Summer 7 Code: 17 6 (i) Differene pure ending and ordinary ending ure ending a) n pure ending the eam deflets into an ar of irle. ) eam is sujeted to normal (ending )stresses of tensile or ompressive in nature Ordinary ending a) n ordinary ending eam dose not deflets into an ar of irle. ) eam is sujeted to normal and shear stresses in it 0 (ii) The equation of torque transmitted y the O.C. shaft a) ased on angle Twist: T G.θ = L G.θ T= L ) ased on shear stress: T q = R q T= R Where, T = Torque ating on shaft (N-mm) R = Radius of urvature shaft (mm) G = Modulus of rigidity (N/mm ) L = Length of shaft (mm) = olar M.. of shaft setion (mm ) = ngle of twist in radians q = Max. shear stress at outer most fire of shaft (N/mm ) age /

Sub. Code:

Sub. Code: Important Instructions to examiners: ) The answers should be examined by key words and not as word-to-word as given in the model answer scheme. ) The model answer and the answer written by candidate may

More information

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A (2 Marks) 1. Define longitudinal strain and lateral strain. 2. State Hooke s law. 3. Define modular ratio,

More information

Torsion. Torsion is a moment that twists/deforms a member about its longitudinal axis

Torsion. Torsion is a moment that twists/deforms a member about its longitudinal axis Mehanis of Solids I Torsion Torsional loads on Cirular Shafts Torsion is a moment that twists/deforms a member about its longitudinal axis 1 Shearing Stresses due to Torque o Net of the internal shearing

More information

mportant nstructions to examiners: ) The answers should be examined by key words and not as word-to-word as given in the model answer scheme. ) The model answer and the answer written by candidate may

More information

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A DEPARTMENT: CIVIL SUBJECT CODE: CE2201 QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A (2 Marks) 1. Define longitudinal strain and lateral strain. 2. State

More information

TORSION By Prof. Ahmed Amer

TORSION By Prof. Ahmed Amer ORSION By Prof. Ahmed Amer orque wisting moments or torques are fores ating through distane so as to promote rotation. Example Using a wrenh to tighten a nut in a bolt. If the bolt, wrenh and fore are

More information

Sample Question Paper

Sample Question Paper Scheme I Sample Question Paper Program Name : Mechanical Engineering Program Group Program Code : AE/ME/PG/PT/FG Semester : Third Course Title : Strength of Materials Marks : 70 Time: 3 Hrs. Instructions:

More information

Lecture 11 Buckling of Plates and Sections

Lecture 11 Buckling of Plates and Sections Leture Bukling of lates and Setions rolem -: A simpl-supported retangular plate is sujeted to a uniaxial ompressive load N, as shown in the sketh elow. a 6 N N a) Calulate and ompare ukling oeffiients

More information

OUTLINE. CHAPTER 7: Flexural Members. Types of beams. Types of loads. Concentrated load Distributed load. Moment

OUTLINE. CHAPTER 7: Flexural Members. Types of beams. Types of loads. Concentrated load Distributed load. Moment OUTLINE CHTER 7: Fleural embers -Tpes of beams, loads and reations -Shear fores and bending moments -Shear fore and bending - -The fleure formula -The elasti urve -Slope and defletion b diret integration

More information

3 Hours/100 Marks Seat No.

3 Hours/100 Marks Seat No. *17304* 17304 14115 3 Hours/100 Marks Seat No. Instructions : (1) All questions are compulsory. (2) Illustrate your answers with neat sketches wherever necessary. (3) Figures to the right indicate full

More information

Beam Stresses Bending and Shear

Beam Stresses Bending and Shear Beam Stresses Bending and Shear Notation: A = name or area A web = area o the web o a wide lange setion b = width o a retangle = total width o material at a horizontal setion = largest distane rom the

More information

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM - 613 403 - THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK Sub : Strength of Materials Year / Sem: II / III Sub Code : MEB 310

More information

UNIT-I STRESS, STRAIN. 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2

UNIT-I STRESS, STRAIN. 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2 UNIT-I STRESS, STRAIN 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2 Young s modulus E= 2 x10 5 N/mm 2 Area1=900mm 2 Area2=400mm 2 Area3=625mm

More information

Mechanics of Structure

Mechanics of Structure S.Y. Diploma : Sem. III [CE/CS/CR/CV] Mechanics of Structure Time: Hrs.] Prelim Question Paper Solution [Marks : 70 Q.1(a) Attempt any SIX of the following. [1] Q.1(a) Define moment of Inertia. State MI

More information

Compression Members Local Buckling and Section Classification

Compression Members Local Buckling and Section Classification Compression Memers Loal Bukling and Setion Classifiation Summary: Strutural setions may e onsidered as an assemly of individual plate elements. Plate elements may e internal (e.g. the wes of open eams

More information

R13. II B. Tech I Semester Regular Examinations, Jan MECHANICS OF SOLIDS (Com. to ME, AME, AE, MTE) PART-A

R13. II B. Tech I Semester Regular Examinations, Jan MECHANICS OF SOLIDS (Com. to ME, AME, AE, MTE) PART-A SET - 1 II B. Tech I Semester Regular Examinations, Jan - 2015 MECHANICS OF SOLIDS (Com. to ME, AME, AE, MTE) Time: 3 hours Max. Marks: 70 Note: 1. Question Paper consists of two parts (Part-A and Part-B)

More information

Strength of Materials

Strength of Materials Strength of Materials Session Pure Bending 04 Leture note : Praudianto, M.Eng. g{ V ä Ä tçw ÄtÇÇ Çz XÇz ÇÜ Çz Xwâvtà ÉÇ WÑtÜàÅÇà g{ V ä Ä tçw ÄtÇÇ Çz XÇz ÇÜ Çz Xwâvtà ÉÇ WÑtÜàÅÇà Pure Bending: Prisati

More information

SRI CHANDRASEKHARENDRA SARASWATHI VISWA MAHAVIDHYALAYA

SRI CHANDRASEKHARENDRA SARASWATHI VISWA MAHAVIDHYALAYA SRI CHANDRASEKHARENDRA SARASWATHI VISWA MAHAVIDHYALAYA (Declared as Deemed-to-be University under Section 3 of the UGC Act, 1956, Vide notification No.F.9.9/92-U-3 dated 26 th May 1993 of the Govt. of

More information

WRAP-AROUND GUSSET PLATES

WRAP-AROUND GUSSET PLATES WRAP-AROUND GUSSET PLATES Where a horizontal brae is loated at a beam-to-olumn intersetion, the gusset plate must be ut out around the olumn as shown in Figure. These are alled wrap-around gusset plates.

More information

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation.

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation. UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation. At the same time the body resists deformation. The magnitude

More information

NON-LINEAR BENDING CHARACTERISTICS OF PHC PILES UNDER VARYING AXIAL LOAD

NON-LINEAR BENDING CHARACTERISTICS OF PHC PILES UNDER VARYING AXIAL LOAD 13 th World Conferene on Earthquake Engineering Vanouver, B.C., Canada August 1-6, 24 aper No. 356 NON-LINEAR BENDING CHARACTERISTICS OF HC ILES UNDER VARYING AXIAL LOAD Toshihiko ASO 1 Fusanori MIURA

More information

LECTURE 2 Geometrical Properties of Rod Cross Sections (Part 2) 1 Moments of Inertia Transformation with Parallel Transfer of Axes.

LECTURE 2 Geometrical Properties of Rod Cross Sections (Part 2) 1 Moments of Inertia Transformation with Parallel Transfer of Axes. V. DEMENKO MECHNCS OF MTERLS 05 LECTURE Geometrial Properties of Rod Cross Setions (Part ) Moments of nertia Transformation with Parallel Transfer of xes. Parallel-xes Theorems S Given: a b = S = 0. z

More information

SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS

SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS Time Allowed:2 Hours Maximum Marks: 300 Attention: 1. Paper consists of Part A (Civil & Structural) Part B (Electrical) and Part C (Mechanical)

More information

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR:

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR: MECHANICS OF STRUCTURES- ASSIGNMENT NO 1 SEMESTER: V 1) Find the least moment of Inertia about the centroidal axes X-X and Y-Y of an unequal angle section 125 mm 75 mm 10 mm as shown in figure 2) Determine

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHAPER MECHANICS OF MAERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John. DeWolf orsion Leture Notes: J. Walt Oler exas eh University 006 he MGraw-Hill Companies, In. All rights reserved. Contents

More information

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy Stress Analysis Lecture 3 ME 276 Spring 2017-2018 Dr./ Ahmed Mohamed Nagib Elmekawy Axial Stress 2 Beam under the action of two tensile forces 3 Beam under the action of two tensile forces 4 Shear Stress

More information

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics Page1 PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [2910601] Introduction, Fundamentals of Statics 1. Differentiate between Scalar and Vector quantity. Write S.I.

More information

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV UNIT I STRESS, STRAIN DEFORMATION OF SOLIDS PART A (2 MARKS)

More information

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains STRENGTH OF MATERIALS-I Unit-1 Simple stresses and strains 1. What is the Principle of surveying 2. Define Magnetic, True & Arbitrary Meridians. 3. Mention different types of chains 4. Differentiate between

More information

2. Determine the deflection at C of the beam given in fig below. Use principal of virtual work. W L/2 B A L C

2. Determine the deflection at C of the beam given in fig below. Use principal of virtual work. W L/2 B A L C CE-1259, Strength of Materials UNIT I STRESS, STRAIN DEFORMATION OF SOLIDS Part -A 1. Define strain energy density. 2. State Maxwell s reciprocal theorem. 3. Define proof resilience. 4. State Castigliano

More information

CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR

CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR 2014-2015 UNIT - 1 STRESS, STRAIN AND DEFORMATION OF SOLIDS PART- A 1. Define tensile stress and tensile strain. The stress induced

More information

Bending stress strain of bar exposed to bending moment

Bending stress strain of bar exposed to bending moment Elastiit and Plastiit Bending stress strain of ar eposed to ending moment Basi priniples and onditions of solution Calulation of ending (diret) stress Design of ar eposed to ending moment Comined stress

More information

Shear Force and Bending Moment

Shear Force and Bending Moment Shear Fore and Bending oent Shear Fore: is the algebrai su of the vertial fores ating to the left or right of a ut setion along the span of the bea Bending oent: is the algebrai su of the oent of the fores

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 006 The Graw-Hill Copanies, n. ll rights reserved. Fourth E CHTER ure ECHNCS OF TERLS Ferdinand. Beer E. Russell Johnston, Jr. John T. DeWolf Bending Leture Notes: J. Walt Oler Teas Teh Universit ECHNCS

More information

PES Institute of Technology

PES Institute of Technology PES Institute of Technology Bangalore south campus, Bangalore-5460100 Department of Mechanical Engineering Faculty name : Madhu M Date: 29/06/2012 SEM : 3 rd A SEC Subject : MECHANICS OF MATERIALS Subject

More information

Structural Analysis I Chapter 4 - Torsion TORSION

Structural Analysis I Chapter 4 - Torsion TORSION ORSION orsional stress results from the action of torsional or twisting moments acting about the longitudinal axis of a shaft. he effect of the application of a torsional moment, combined with appropriate

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 00 The Graw-Hill Copanies, n. All rights reserved. Third E CHAPTER Pure ECHANCS OF ATERALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Bending Leture Notes: J. Walt Oler Teas Teh Universit

More information

2 Axially Loaded Numbers

2 Axially Loaded Numbers xially oaded Numers hanges in engths of xially oaded Memers rolem.-1 The T-shaped arm shown in the figure lies in a vertical plane and pivots aout a horizontal pin at. The arm has constant cross-sectional

More information

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS Name :. Roll No. :..... Invigilator s Signature :.. 2011 SOLID MECHANICS Time Allotted : 3 Hours Full Marks : 70 The figures in the margin indicate full marks. Candidates are required to give their answers

More information

Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames

Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames IL 32 /9 ppling the virtual work equations to a frame struture is as simple as separating the frame into a series of beams and summing the virtual work for eah setion. In addition, when evaluating the

More information

Case Study in Reinforced Concrete adapted from Simplified Design of Concrete Structures, James Ambrose, 7 th ed.

Case Study in Reinforced Concrete adapted from Simplified Design of Concrete Structures, James Ambrose, 7 th ed. ARCH 631 Note Set 11 F015abn Case Study in Reinfored Conrete adapted from Simplified Design of Conrete Strutures, James Ambrose, 7 th ed. Building desription The building is a three-story offie building

More information

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC.

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC. BENDING STRESS The effect of a bending moment applied to a cross-section of a beam is to induce a state of stress across that section. These stresses are known as bending stresses and they act normally

More information

Downloaded from Downloaded from / 1

Downloaded from   Downloaded from   / 1 PURWANCHAL UNIVERSITY III SEMESTER FINAL EXAMINATION-2002 LEVEL : B. E. (Civil) SUBJECT: BEG256CI, Strength of Material Full Marks: 80 TIME: 03:00 hrs Pass marks: 32 Candidates are required to give their

More information

18.Define the term modulus of resilience. May/June Define Principal Stress. 20. Define Hydrostatic Pressure.

18.Define the term modulus of resilience. May/June Define Principal Stress. 20. Define Hydrostatic Pressure. CE6306 STREGNTH OF MATERIALS Question Bank Unit-I STRESS, STRAIN, DEFORMATION OF SOLIDS PART-A 1. Define Poison s Ratio May/June 2009 2. What is thermal stress? May/June 2009 3. Estimate the load carried

More information

BEHAVIOR OF SQUARE CONCRETE-FILLED TUBULAR COLUMNS UNDER ECCENTRIC COMPRESSION WITH DOUBLE CURVATURE DEFLECTION

BEHAVIOR OF SQUARE CONCRETE-FILLED TUBULAR COLUMNS UNDER ECCENTRIC COMPRESSION WITH DOUBLE CURVATURE DEFLECTION Otober 2-7, 28, Beijing, China BEHAVIOR OF SQARE CONCRETE-FILLED TBLAR COLNS NDER ECCENTRIC COPRESSION WITH DOBLE CRVATRE DEFLECTION T. Fujinaga, H. Doi 2 and Y.P. Sun 3 Assoiate Professor, Researh Center

More information

Only for Reference Page 1 of 18

Only for Reference  Page 1 of 18 Only for Reference www.civilpddc2013.weebly.com Page 1 of 18 Seat No.: Enrolment No. GUJARAT TECHNOLOGICAL UNIVERSITY PDDC - SEMESTER II EXAMINATION WINTER 2013 Subject Code: X20603 Date: 26-12-2013 Subject

More information

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1 UNIT I STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define: Stress When an external force acts on a body, it undergoes deformation. At the same time the body resists deformation. The

More information

2. Polar moment of inertia As stated above, the polar second moment of area, J is defined as. Sample copy

2. Polar moment of inertia As stated above, the polar second moment of area, J is defined as. Sample copy GATE PATHSHALA - 91. Polar moment of inertia As stated above, the polar second moment of area, is defined as z π r dr 0 R r π R π D For a solid shaft π (6) QP 0 π d Solid shaft π d Hollow shaft, " ( do

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 00 The Graw-Hill Copanies, n. All rights reserved. Third E CHAPTER 4 Pure ECHANCS OF ATERALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Bending Leture Notes: J. Walt Oler Teas Teh Universit

More information

CIVL222 STRENGTH OF MATERIALS. Chapter 6. Torsion

CIVL222 STRENGTH OF MATERIALS. Chapter 6. Torsion CIVL222 STRENGTH OF MATERIALS Chapter 6 Torsion Definition Torque is a moment that tends to twist a member about its longitudinal axis. Slender members subjected to a twisting load are said to be in torsion.

More information

1. INTRODUCTION. l t t r. h t h w. t f t w. h p h s. d b D F. b b d c. L D s

1. INTRODUCTION. l t t r. h t h w. t f t w. h p h s. d b D F. b b d c. L D s Rapid Assessment of Seismi Safety of Elevated ater Tanks with FRAME Staging 1. NTRODUCTON 1.1 ntrodution ater tanks are lifeline items in the aftermath of earthquakes. The urrent pratie of designing elevated

More information

2014 MECHANICS OF MATERIALS

2014 MECHANICS OF MATERIALS R10 SET - 1 II. Tech I Semester Regular Examinations, March 2014 MEHNIS OF MTERILS (ivil Engineering) Time: 3 hours Max. Marks: 75 nswer any FIVE Questions ll Questions carry Equal Marks ~~~~~~~~~~~~~~~~~~~~~~~~~

More information

Buckling loads of columns of regular polygon cross-section with constant volume and clamped ends

Buckling loads of columns of regular polygon cross-section with constant volume and clamped ends 76 Bukling loads of olumns of regular polygon ross-setion with onstant volume and lamped ends Byoung Koo Lee Dept. of Civil Engineering, Wonkwang University, Iksan, Junuk, 7-79, Korea Email: kleest@wonkwang.a.kr

More information

Design of Steel Structures Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar

Design of Steel Structures Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar 5.10 Examples 5.10.1 Analysis of effective section under compression To illustrate the evaluation of reduced section properties of a section under axial compression. Section: 00 x 80 x 5 x 4.0 mm Using

More information

The problem of transmitting a torque or rotary motion from one plane to another is frequently encountered in machine design.

The problem of transmitting a torque or rotary motion from one plane to another is frequently encountered in machine design. CHAPER ORSION ORSION orsion refers to the twisting of a structural member when it is loaded by moments/torques that produce rotation about the longitudinal axis of the member he problem of transmitting

More information

Beams on Elastic Foundation

Beams on Elastic Foundation Professor Terje Haukaas University of British Columbia, Vanouver www.inrisk.ub.a Beams on Elasti Foundation Beams on elasti foundation, suh as that in Figure 1, appear in building foundations, floating

More information

BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS)

BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS) BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS) All questions carry equal marks(10 marks) Q.1 (a) Write the SI units of following quantities and also mention whether it is scalar or vector: (i)

More information

Design of AAC floor slabs according to EN 12602

Design of AAC floor slabs according to EN 12602 Design of AAC floor slabs aording to EN 160 Example 1: Floor slab with uniform load 1.1 Issue Design of a floor slab under a living room Materials Component with a ompressive strength lass AAC 4,5, densit

More information

IVIL.COM, C. English - Arabic. Arrow Assume Assumption Available Average Axes Axial Axis

IVIL.COM, C. English - Arabic. Arrow Assume Assumption Available Average Axes Axial Axis Abrupt Action Accuracy Accurate Advantage Algebra Algebraic Algebraic equation English - Arabic Algebraic expression Algebraic sum Allow Allowable Ambiguous Analyze Analysis f sections Structural analysis

More information

Wood Design. = theoretical allowed buckling stress

Wood Design. = theoretical allowed buckling stress Wood Design Notation: a = name for width dimension A = name for area A req d-adj = area required at allowable stress when shear is adjusted to inlude self weight b = width of a retangle = name for height

More information

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad -00 04 CIVIL ENGINEERING QUESTION BANK Course Name : STRENGTH OF MATERIALS II Course Code : A404 Class : II B. Tech II Semester Section

More information

RC DEEP BEAMS ANALYSIS CONSIDERING LOCALIZATION IN COMPRESSION

RC DEEP BEAMS ANALYSIS CONSIDERING LOCALIZATION IN COMPRESSION RC DEEP BEAMS ANAYSIS CONSIDERING OCAIZATION IN COMPRESSION Manakan ERTSAMATTIYAKU* 1, Torsak ERTSRISAKURAT* 1, Tomohiro MIKI* 1 and Junihiro NIWA* ABSTRACT: It has been found that RC deep beams usually

More information

FIXED BEAMS IN BENDING

FIXED BEAMS IN BENDING FIXED BEAMS IN BENDING INTRODUCTION Fixed or built-in beams are commonly used in building construction because they possess high rigidity in comparison to simply supported beams. When a simply supported

More information

IN-PLANE VIBRATIONS OF CURVED BEAMS WITH VARIABLE CROSS-SECTIONS CARRYING ADDITIONAL MASS

IN-PLANE VIBRATIONS OF CURVED BEAMS WITH VARIABLE CROSS-SECTIONS CARRYING ADDITIONAL MASS 11 th International Conferene on Vibration Problems Z. Dimitrovová et al. (eds.) Lisbon, Portugal, 9-1 September 013 IN-PLANE VIBRATIONS OF CURVED BEAMS WITH VARIABLE CROSS-SECTIONS CARRYING ADDITIONAL

More information

SN QUESTION YEAR MARK 1. State and prove the relationship between shearing stress and rate of change of bending moment at a section in a loaded beam.

SN QUESTION YEAR MARK 1. State and prove the relationship between shearing stress and rate of change of bending moment at a section in a loaded beam. ALPHA COLLEGE OF ENGINEERING AND TECHNOLOGY DEPARTMENT OF MECHANICAL ENGINEERING MECHANICS OF SOLIDS (21000) ASSIGNMENT 1 SIMPLE STRESSES AND STRAINS SN QUESTION YEAR MARK 1 State and prove the relationship

More information

MARKS DISTRIBUTION AS PER CHAPTER (QUESTION ASKED IN GTU EXAM) Name Of Chapter. Applications of. Friction. Centroid & Moment.

MARKS DISTRIBUTION AS PER CHAPTER (QUESTION ASKED IN GTU EXAM) Name Of Chapter. Applications of. Friction. Centroid & Moment. Introduction Fundamentals of statics Applications of fundamentals of statics Friction Centroid & Moment of inertia Simple Stresses & Strain Stresses in Beam Torsion Principle Stresses DEPARTMENT OF CIVIL

More information

2012 MECHANICS OF SOLIDS

2012 MECHANICS OF SOLIDS R10 SET - 1 II B.Tech II Semester, Regular Examinations, April 2012 MECHANICS OF SOLIDS (Com. to ME, AME, MM) Time: 3 hours Max. Marks: 75 Answer any FIVE Questions All Questions carry Equal Marks ~~~~~~~~~~~~~~~~~~~~~~

More information

Two-Way Flat Slab (Concrete Floor with Drop Panels) System Analysis and Design

Two-Way Flat Slab (Concrete Floor with Drop Panels) System Analysis and Design Two-Way Flat Slab (Conrete Floor with Drop Panels) System Analysis and Design Two-Way Flat Slab (Conrete Floor with Drop Panels) System Analysis and Design Design the onrete floor slab system shown below

More information

N = Shear stress / Shear strain

N = Shear stress / Shear strain UNIT - I 1. What is meant by factor of safety? [A/M-15] It is the ratio between ultimate stress to the working stress. Factor of safety = Ultimate stress Permissible stress 2. Define Resilience. [A/M-15]

More information

Software Verification

Software Verification EC-4-004 Example-001 STEEL DESIGNERS MANUAL SEVENTH EDITION - DESIGN OF SIMPLY SUPPORTED COMPOSITE BEAM EXAMPLE DESCRIPTION Consider an internal seondary omposite beam of 1-m span between olumns and subjet

More information

Shafts. Fig.(4.1) Dr. Salah Gasim Ahmed YIC 1

Shafts. Fig.(4.1) Dr. Salah Gasim Ahmed YIC 1 Shafts. Power transmission shafting Continuous mechanical power is usually transmitted along and etween rotating shafts. The transfer etween shafts is accomplished y gears, elts, chains or other similar

More information

The casing is subjected to the following:

The casing is subjected to the following: 16.50 Leture 13 Subjet: Roket asing design; Strutural modeling Thus far all our modeling has dealt with the fluid mehanis and thermodynamis of rokets. This is appropriate beause it is these features that

More information

STRESS, STRAIN AND DEFORMATION OF SOLIDS

STRESS, STRAIN AND DEFORMATION OF SOLIDS VELAMMAL COLLEGE OF ENGINEERING AND TECHNOLOGY, MADURAI 625009 DEPARTMENT OF CIVIL ENGINEERING CE8301 STRENGTH OF MATERIALS I -------------------------------------------------------------------------------------------------------------------------------

More information

BEAMS: SHEARING STRESS

BEAMS: SHEARING STRESS LECTURE Third Edition BEAMS: SHEARNG STRESS A. J. Clark Shool of Engineering Department of Civil and Environmental Engineering 14 Chapter 6.1 6.4 b Dr. brahim A. Assakkaf SPRNG 200 ENES 220 Mehanis of

More information

DEPARTMENT OF CIVIL ENGINEERING

DEPARTMENT OF CIVIL ENGINEERING KINGS COLLEGE OF ENGINEERING DEPARTMENT OF CIVIL ENGINEERING SUBJECT: CE 2252 STRENGTH OF MATERIALS UNIT: I ENERGY METHODS 1. Define: Strain Energy When an elastic body is under the action of external

More information

UNIT III DEFLECTION OF BEAMS 1. What are the methods for finding out the slope and deflection at a section? The important methods used for finding out the slope and deflection at a section in a loaded

More information

MAHALAKSHMI ENGINEERING COLLEGE

MAHALAKSHMI ENGINEERING COLLEGE MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAALLI - 6113. QUESTION WITH ANSWERS DEARTMENT : CIVIL SEMESTER: V SUB.CODE/ NAME: CE 5 / Strength of Materials UNIT 3 COULMNS ART - A ( marks) 1. Define columns

More information

Stress triaxiality to evaluate the effective distance in the volumetric approach in fracture mechanics

Stress triaxiality to evaluate the effective distance in the volumetric approach in fracture mechanics IOSR Journal of ehanial and Civil Engineering (IOSR-JCE) e-issn: 78-1684,p-ISSN: 30-334X, Volume 11, Issue 6 Ver. IV (Nov- De. 014), PP 1-6 Stress triaxiality to evaluate the effetive distane in the volumetri

More information

Government of Karnataka Department of Technical Education Board of Technical Examinations, Bangalore

Government of Karnataka Department of Technical Education Board of Technical Examinations, Bangalore CIE- 25 Marks Government of Karnataka Department of Technical Education Board of Technical Examinations, Bangalore Course Title: STRENGTH OF MATERIALS Course Code: Scheme (L:T:P) : 4:0:0 Total Contact

More information

DESIGN OF BEAMS AND SHAFTS

DESIGN OF BEAMS AND SHAFTS DESIGN OF EAMS AND SHAFTS! asis for eam Design! Stress Variations Throughout a Prismatic eam! Design of pristmatic beams! Steel beams! Wooden beams! Design of Shaft! ombined bending! Torsion 1 asis for

More information

Module 2 Stresses in machine elements. Version 2 ME, IIT Kharagpur

Module 2 Stresses in machine elements. Version 2 ME, IIT Kharagpur Module Stresses in machine elements Lesson Compound stresses in machine parts Instructional Objectives t the end of this lesson, the student should be able to understand Elements of force system at a beam

More information

Two-Way Concrete Floor Slab with Beams Design and Detailing (CSA A )

Two-Way Concrete Floor Slab with Beams Design and Detailing (CSA A ) Two-Way Conrete Floor Slab with Beams Design and Detailing (CSA A.-14) Two-Way Conrete Floor Slab with Beams Design and Detailing (CSA A.-14) Design the slab system shown in Figure 1 for an intermediate

More information

Mechanics of Materials II. Chapter III. A review of the fundamental formulation of stress, strain, and deflection

Mechanics of Materials II. Chapter III. A review of the fundamental formulation of stress, strain, and deflection Mechanics of Materials II Chapter III A review of the fundamental formulation of stress, strain, and deflection Outline Introduction Assumtions and limitations Axial loading Torsion of circular shafts

More information

ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING

ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING QUESTION BANK FOR THE MECHANICS OF MATERIALS-I 1. A rod 150 cm long and of diameter 2.0 cm is subjected to an axial pull of 20 kn. If the modulus

More information

Advanced Structural Analysis EGF Section Properties and Bending

Advanced Structural Analysis EGF Section Properties and Bending Advanced Structural Analysis EGF316 3. Section Properties and Bending 3.1 Loads in beams When we analyse beams, we need to consider various types of loads acting on them, for example, axial forces, shear

More information

STRESS. Bar. ! Stress. ! Average Normal Stress in an Axially Loaded. ! Average Shear Stress. ! Allowable Stress. ! Design of Simple Connections

STRESS. Bar. ! Stress. ! Average Normal Stress in an Axially Loaded. ! Average Shear Stress. ! Allowable Stress. ! Design of Simple Connections STRESS! Stress Evisdom! verage Normal Stress in an xially Loaded ar! verage Shear Stress! llowable Stress! Design of Simple onnections 1 Equilibrium of a Deformable ody ody Force w F R x w(s). D s y Support

More information

2. The Energy Principle in Open Channel Flows

2. The Energy Principle in Open Channel Flows . The Energy Priniple in Open Channel Flows. Basi Energy Equation In the one-dimensional analysis of steady open-hannel flow, the energy equation in the form of Bernoulli equation is used. Aording to this

More information

(48) CHAPTER 3: TORSION

(48) CHAPTER 3: TORSION (48) CHAPTER 3: TORSION Introduction: In this chapter structural members and machine parts that are in torsion will be considered. More specifically, you will analyze the stresses and strains in members

More information

2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at A and supported at B by rod (1). What is the axial force in rod (1)?

2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at A and supported at B by rod (1). What is the axial force in rod (1)? IDE 110 S08 Test 1 Name: 1. Determine the internal axial forces in segments (1), (2) and (3). (a) N 1 = kn (b) N 2 = kn (c) N 3 = kn 2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at

More information

OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS. You should judge your progress by completing the self assessment exercises. CONTENTS

OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS. You should judge your progress by completing the self assessment exercises. CONTENTS Unit 2: Unit code: QCF Level: 4 Credit value: 15 Engineering Science L/601/1404 OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS 1. Be able to determine the behavioural characteristics of elements of static engineering

More information

: APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE

: APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE MODULE TOPIC PERIODS 1 Simple stresses

More information

A.1. Member capacities A.2. Limit analysis A.2.1. Tributary weight.. 7. A.2.2. Calculations. 7. A.3. Direct design 13

A.1. Member capacities A.2. Limit analysis A.2.1. Tributary weight.. 7. A.2.2. Calculations. 7. A.3. Direct design 13 APPENDIX A APPENDIX A Due to its extension, the dissertation ould not inlude all the alulations and graphi explanantions whih, being not essential, are neessary to omplete the researh. This appendix inludes

More information

Torsion Stresses in Tubes and Rods

Torsion Stresses in Tubes and Rods Torsion Stresses in Tubes and Rods This initial analysis is valid only for a restricted range of problem for which the assumptions are: Rod is initially straight. Rod twists without bending. Material is

More information

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method Slenderness Effets for Conrete Columns in Sway Frame - Moment Magnifiation Method Slender Conrete Column Design in Sway Frame Buildings Evaluate slenderness effet for olumns in a sway frame multistory

More information

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3.

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3. ES230 STRENGTH OF MTERILS Exam 3 Study Guide Exam 3: Wednesday, March 8 th in-class Updated 3/3/17 Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on

More information

Uniaxial Concrete Material Behavior

Uniaxial Concrete Material Behavior COMPUTERS AND STRUCTURES, INC., JULY 215 TECHNICAL NOTE MODIFIED DARWIN-PECKNOLD 2-D REINFORCED CONCRETE MATERIAL MODEL Overview This tehnial note desribes the Modified Darwin-Peknold reinfored onrete

More information

Lab Exercise #3: Torsion

Lab Exercise #3: Torsion Lab Exercise #3: Pre-lab assignment: Yes No Goals: 1. To evaluate the equations of angular displacement, shear stress, and shear strain for a shaft undergoing torsional stress. Principles: testing of round

More information

Part G-4: Sample Exams

Part G-4: Sample Exams Part G-4: Sample Exams 1 Cairo University M.S.: Eletronis Cooling Faulty of Engineering Final Exam (Sample 1) Mehanial Power Engineering Dept. Time allowed 2 Hours Solve as muh as you an. 1. A heat sink

More information

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method Slenderness Effets for Conrete Columns in Sway Frame - Moment Magnifiation Method Slender Conrete Column Design in Sway Frame Buildings Evaluate slenderness effet for olumns in a sway frame multistory

More information

M. Vable Mechanics of Materials: Chapter 5. Torsion of Shafts

M. Vable Mechanics of Materials: Chapter 5. Torsion of Shafts Torsion of Shafts Shafts are structural members with length significantly greater than the largest cross-sectional dimension used in transmitting torque from one plane to another. Learning objectives Understand

More information