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Solution HW2 - Spring2023

The document contains a series of engineering problems related to the tensile properties of materials, including calculations for force, stress, and deflection in various scenarios involving steel, brass, and aluminum rods. Each problem provides specific parameters such as length, diameter, and applied loads, requiring the determination of mechanical properties like modulus of elasticity and stress. The problems illustrate applications in structural engineering and material science, emphasizing the importance of understanding material behavior under load.

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0% found this document useful (0 votes)
71 views12 pages

Solution HW2 - Spring2023

The document contains a series of engineering problems related to the tensile properties of materials, including calculations for force, stress, and deflection in various scenarios involving steel, brass, and aluminum rods. Each problem provides specific parameters such as length, diameter, and applied loads, requiring the determination of mechanical properties like modulus of elasticity and stress. The problems illustrate applications in structural engineering and material science, emphasizing the importance of understanding material behavior under load.

Uploaded by

ammarnakhi
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
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An 18-m-long steel wire of S-mm diameter is to be used in the manufacture of a prestressed conerete beam. It is observed that the wire stretches 45 mm when a tensile force P is applied. Knowing that £ = 200 GPa, determine (a) the magnitude of the force P, (b) the corresponding normal stress in the wire. @ aL : Pp. EAA EA a . Pe 2000 © «YG (SY mye US win sO \BRIO™ mys « Pe 437.4370) -/Pe 9.32 1) © £-P . TwiFYaN NMG eye Seo Wra (1) Wy m ! PROBLEM 2.7 2.7 A steel rod is 2.2 m long and must not stretch more than 1.2 mm when a 8.5 KN load is applied to it. Knowing that E = 200 GPa, determine (a) the smallest diameter rod which should be used, (b) the corresponding normal stress caused by the load. @, _ PL ” ER > P © 6-f- _ &: Sx) ¥ 2- 2x0 min Zeopid PD. oy a mn™ AZ 9-16 mm SHO A) “Wy (7 9) mm? < 2mm 109-| HP (7) PROBLEM 2.15 A single axial load of magnitude P =58 kN is applied at end C of the brass rod ABC. Knowing that £ = 105 GPa, determine the diameter d of portion BC for which the deflection of point C will be 3 mm. SB IEN) $= 53K) j ’ ac 5 > 2m ogm D ae —> go ‘ > > Ben | —> Pa, = 53 ta) a A B > °s c= Bejy = Legtb wa =+3inm 3 4 53x10 x Foo . SBxI0 % 1200 co /05x1OxtA* BRIO 30° pd = 16.52 mm r=4¢p) PROBLEM 219 Both portions of the rod ABC are made of an aluminum for which £ =70 GPa. Knowi neat he rms ar KN, determine (the ae of Q 30 hat the deflect 0, (b) th reter DO ter 2 | Yii-O) 9 @ am Boje- Maye rd, Ble sth, =+ nee 18 wo \ (CO pins ae WT 29|Q = 32-3 Vf (4-9) 2 _ ( 4-323) y0x >) P= 4-9) © 4g Bee PonsbT bot =- 0.073 mm i.e. |Op- 0-073 mm (| )(Ghrlenia) | bea) = ae Rf PROBLEM 2.23 Members 4B and BC are, made of steel (E = 200 GPa) with cross- ectional areas of 516 mm” and 412 mm’, respectively. For the loading shown, determine the elongation of (a) member AB, (5) member BC. => Vne= 195-260 (1) * joi, “B's ZY¥x=° BIAS > Ve = Wee Fy iB) oA) es => Vee- (5om() 19S an6ae (58 122 | * 2 200,00 T x Sib mn ER Jag 20000 ox Slim SOR Don. 1s I B x00 mn Oe be. Zeon TH mt | rN @Lhoe O4ec- _. . ef se s r Ze => 195 = Tag cs) . VS __ Tes Dd 4/4 mn =(incresein teenth) =| 3-23 mm Cee) PROBLEM 2.27 A D P=5kN Each of the links 4B and CD is made of aluminum (E = 75 GPa) and has Te a cross-sectional area of 258 mm’, Knowing that they support the rigid E member BC, determine the deflection of point £. Fd nam —° 0.20 m he Ska) 3 Ze ‘ - => Fan(o-z+0-4u) B = S(O) => Sap 2 344K CY Z¥ge0 => Kep 2 2-344 = 1-56 ke (7) Ap = Ap ems = 2-064 mm (4) he = hep, (gp bipasies Sas) = 0-024 mm (J) o-2m o-44mm E ca BSp-Ac - Ag-Ae é f Bp-A 6 >A, (ABB oa 4Ag =| 0-053 mm aN o2m E o-44m PROBLEM 2.61 ‘A 20-mm-diameter rod made of an experimental plastic is subjected to a tensile force of magnitude P = 6 KN. Knowing that an elongation of 14 mm and a decrease in diameter of 0.85 mm are observed in a 150-mm length, determine the modulus of elasticity, the modulus ot iy, and Poisson’ ratio for the material. 9 _. Lien) SA ‘a0 mn mn — OL +l mm. 32 ~)0 > wm te TD /g01r0m ¥ I8-32790 mein Ze _ Sd ~~ O:3Sm S425 KJ" rom ym ~ “dy zoom" _ Ct 865 =|0.455 -e - "93-33% yp bxion) = (9. 6) 2 YA 7 Wy (os nn? A 1 MR (1) ba EG = [el SIN popes : ‘7 9333x0° | He Ble E_ 2 2046S Wh —— - , Z(H) 27+ 0-455) ae ° oo A line of slope 4:10 has been scribed on a cold-rolled yellow-brass 20. wow | 150 mum | plate, 150:mm wide and 6 mm thick. Knowing that £ = 105 GPa and ————*__ y= 0.34, determine the slope of the line when the plate is subjected to a 200-KN centric axial load as shown. J Zoo cn 2g —_ "Ihe = wm jo 200 x10 1) orem - — = 222.22 TT * Tmt Wa (1) Gye 222122 WW 4712. K10° vam, Cx = Ee yosx07 Pa hey -( Mn) Layo = (14 2:l2ni’) 10 = 10.021 by = -U x= — 034 (+212x0°) =- 042) x0 mys Lyye(regyhy,o = (I4(-0-721 x0) W=3z > ple Slope = a S9AF mo 10-02[ mm —=_ ar PROBLEM 2.69 A 30-mm square was scribed on the side of a large steel pressure vessel. After pressurization, the biaxial stress condition at the square is as shown. For £ = 200 GPa and v =0.30, determine the change in length of (a) side AB, (b) side BC, (c) diagnonal AC. bye + 30 Ra, byae yo Wea , &z=0 Wa ene 56 -ulbys th. = {a- 03(40-+0)f Zp Expat 034 HS? wren ain incyease “5 Ey = AAO Nya 20mm (0:34x06°) =}+J0-2X/0 mm] L460 eye [os veal) Lf yo-05(erra)f => ey =+ 0.03 re ono Knenease. -a\ |Y.,, 4 Gy = Bee = WA ef 0 mm (0-08) 2210 Le, i Lacie [Ladct bac .= | 30430 = 42-4264 Lac, [Legge bee, Re | 30. 102 + 30.0024"= 424353 wn [ML ad = 4D-43$3-A2 YHA T Axo mm PROBLEM 2.75 The plastic block shown is i \ded to a rigid support and to a vertical plate to which a 240-kN load P is applied. Knowing that for the plastic us G=1080 MPa, determine the deflection ofthe plate. 5D mm i __ 2K) | 25 MP, 2 plskic~ Fpo(goyrme Sp boskc “oo Splshe- Doloshic = a N\A = 235 BIx 7 ple SO MPa rad | 5 M40 Bolaheo= & — am Az 50%233IN0- ao Ss] K =14 wld) J SSR NANA — US Each of the four vertical links connecting the two rigid hori zontal. members is os a aluminum (E=70 GPa) and has rectangular tere of 10 x 40 mm. te the loading shown, determine the deflectio of (a) point E, ro 7 (c) point G. a c dD, 4 EFG: J | Za N e7° aoe a > Lleg (4o0)=24 (652) “ 25emm Yoomm AZXy-2 > Fee + 2(19:5) -24=° > Yep= 7-5 = ZOKN) ©) LL ) End asomn NS eN OD mn eels -&) FOpO IE (Yox'0) on Oe x fom a snl yet oS 650 mm oom => Kee O> ZaAG mm xO mm

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