L Table of Average Mechanical Properties of Typical Engineering Materials (SI Units) ll page/mukasuratf

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/ I-INTVERSITI SAINS MALAYSIA First Semester Examination Academic Session 2008/2009 P eperiks aan S em es ter P ert ama Sidang Akademik 2 008/2 009 November 2008 November 2008 EMM 22113- Strength of Materials Kekuutan Bahun Duration : 3 hours Masa : 3 jam INSTRUCTIONS TO CANDIDATE: ARAHAN IGPADA CALON: Please check that this paper contains SEVEN (n printed pages, ONE (1) page appendix and SIX (O questions before you begin the examination. Sila pastikan bahawa kertos soalan ini mengandungi TIIJUH 0l mukssurat bercetak, SATU (1) mukasurat lampiran dan ENAM (61 soalan sebelum anda memulakan peperil<saan. Answer FM ($ questions. Jawab LIMA (5t soalan. Answer all questions in ENGLISH OR BAHASA MALAYSIA OR a combination of both. Calon boleh menjawab semua soalan dalam - BAHASA MALAYSIA ATAU BAHASA INGGERIS ATAU kombinasi kedua-duanya. Each question must begin from a new page. Setiap soalan mestilah dimulakan pada mukasurat yang baru. Appendix/Iampirant L Table of Average Mechanical Properties of Typical Engineering Materials (SI Units) ll page/mukasuratf...2/-

IEMM 22U3] Ql. The 50 mm diameter cylinder is made of Am 1004-T61 magnesium and is placed in the clamp when the temperature is { = 30"C as shown in the Figure Ql. The two 304 stainless steel carriage bolts of the clamp each have a diameter of 10 mm with 20 threads per 20 mm, and they hold the cylinder snug with negligible force against the rigid jaws. In answering the followings, the explanation of whether it is statically determinate problem, the equations of equilibrium and compatibility, the free body diagram and the geometry (diagram) of deformation must be included. Satu silinder magnesium Am 1004-761 berdiameter 50 mm diletakkan antara pengapit pada suhu 4:30'C seperti dalam Rajah 51. Dua bolt pembawa keluli tahan karat 304 pada pengapit, masing-masing berdiameter l0 mm dengan 20 lilitan per 20 mm, dan mereka memegang sendat silinder dimana daya bertindak pada rahang-rahang tegar boleh diabaikan. Semasa menjawab soalan berikut, penerangan sama ada ini masalah penentuan secara statik, persamaan-persamoan keseimbangan dan keserasian, rajah jasad bebas serta-ubah bentuk geometri (rajah) perlu disertakan. Figure Ql Rajah SI lal Using a wrench, each nut is further tightened one full turn. Determine the stresses in bolt and cylinder, and explain whether this o'elastic" analysis is valid or not. Menggunaknn perungkah, setiap nat diketatknn lagi sebanyak satu pusingan. Tentukan tegasan pada bolt dan silinder, serta terangknn sama ada analisis "elastik" ini adalah sah atau tidak. (70 markslmarkah) -2-...3t-

Ibl IEMM 22U3) Then, if the temperature is decreased to Tz =10" C, determine the stresses in bolt and cvlinder. Selepas itu, jika suhu dikurangkan kepada Tz =10'C, tentukan tegasan pada bolt dan silinder. (30 markslmarkah) Q2. The cantilever beam is subjected to the distributed loading and moment Mn shown in Figure Q2. Rasuk julur dikenakan beban teragih dan momen Mo seperti yang ditunjukkan dalam Rajah 52. kl.i/m knm 2.0 m, Figure Q2 Rajah 52 (D Determine the shear force, F and bending moment, M throughout the beam as functions of x. Tentukan daya ricih, F dan momen lentur, M sebagai fungsi x bagi rasuk tersebut. (70 markslmarkah) (id Draw the shear force and bending moment diagrams. Lukiskan rajah daya ricih dan rajah momen lentur. (30 markslmarkah) -3-...41-

IEMM 22U31 Q3. The beam in Figure Q3 is fixed at A and simply supported at B. If it is subjected to the distributed load p, determine the slope and deflection of the beam in term of x, I, p, E and I. Modulus of elasticity and moment of inertia of the beam are E and I, respectively. Rasuk dalam Rajah 53 ditetapkan pada A dan disokong mudah pada B. Jika ia dikenakan beban teragih p, tentukan kecerunan dan pesongan bagi rasuk tersebut dalam sebutan x, l, p, E dan L Modulus elastik dan momen inersia bagi rasuk, masing-masing adalah E dan I. Figure Q3 Rajah 53 (100 markslmarkah) Q4. lal Define the following terms and cite an example for a sketch showing the condition reflecting such case each case together with (D Plane stress (id Plane strain (iii) Principal plane Berikan definisi istilah berikut dan nyatakan satu contoh bagi setiap kes dengan lakaran yang menggambarkan contoh tersebut (i) (i, (ii, Tegasan satah Terikan satah Satah utama (40 markslmarkah\ Ibl For the loading condition shown in thb components below calculate the principal stresses and the maximum shear stress at the point and draw the Mohr's circle representing the stress condition in each point Bagi keadaan tegasan yang ditunjukknn di dalam unsur-unsur di bawah, kirakan tegasan utama dan tegasan riceh utama dan lakarkan Bulatan Mohr yang mewakili keadaan tegasan bagi setiap unsur. -4-...s/-

IEMM 221/31 %o* T- 20Nm Diameter of shaft = 1Omm Figure Q4lbl Raiah s4[b] (60 marks/ markah) Q5. A gear driven pump is shown in Figure Q5. The pump impeller is represented as A and supported by deep groove ball bearings at B and C. The gear is transmitting power from the motor to the shaft of the pump. Assuming that the force from the contact at the gear teeth can be represented by the following force vector : E:700L-700i N And the position vector of the contact point to the centre line of the shaft is given as g = 250/ mm The bearings are assumed to absorb all the radial load and the pump impeller is absorbing all the supplied torque. Determine the minimum radius of a solid shaft suitable for this case when the allowable normal stress is 100 MPa and the allowable shear stress is limited to 60 MPa. -5-...6/-

IEMM 22U3) Sebuah pam yqng dipacu menggunakan gear ditunjukkan di dalam Rajah 55. Pendesak pam di wakili oleh A dan disokong oleh galas bebola di B dan C. Gear tersebut menghantar kuasa daripada motor kepada syaf pam. Andaikan daya yang bertindak pa,da titik sentuh boleh diwakili oleh vektor daya berikut: F:700i-740j N Dan vektor kedudukan titik sentuh diukur daripada garis paksi syaf diberikan oleh vektor berikut : y: 250 j mm Galas bebola dianggap menanggung kesemua bebaban jejarian dan pendesak pam menyerap kesemua kilas yang dihantar oleh syaf. Tentukan jejari minimum bagi syaf padu jika tegasan normal yang dibenarkan ialah 100 MPa dan tegasan riceh yang dibenarkan ialah 60 MPa. * F=700i-700iN Figure Q5 Rajah 55 (100 markslmarknh) -6-...7/-

-7- IEMM 22r/3] Q6. lal For an assembly of a shaft and a disc, the shaft is required to fit into a disc of an outer diameter of 250 mm and inner diameter of 50 mm with thickness of 25 mm. The shaft is solid steel and the disc is also made of steel (E :200 GPa, v:0.28). Determine the following: (D The normal stress at the interface (il) The hoop stress at the interface for the disc. (iii) The normal force at the interface (iv) The force needed to overcome friction to push the shaft into the (v) disc if the friction coefficient at the interface is 0.4 The maximum torque that can be transmitted through the discshaft assembly based on the friction at the interface only Bagi satu pepasong syaf dan cakera di mana syaf di pasong ketat kepada cakera yang mempunyt diameter luaran 250 mm dan diameter dalaman 50 mm dengan ketebalam 25 mm. Syaf padu tersebut di buat daripada keluli (E : 200 GPa, v: 0.28). Tentukan yang berikut: (i) Tegasan normal pada antaramuka (i, Tegasan lingkar pada antaramuka untuk cakera (ii, Daya normal pada antaramuka (iv) Daya yang diperlukan untuk mengatasi geseran apabila syaf ditolak masuk kedalam cakera jika pekali geseran di antara muka ialah 0.4 (v) Kilas mal<simum yang boleh dihantar menerusi pepasang syaf-cakera tersebut berdasarkan geseran pada antaramuka sahaja (80 markslmarkah) lbl Assess suitability of the shaft-disc pair using interference fit to transmit torque when compared to Jhe use of key and keyway as a mean of locating the disc to the shaft when transmitting torque. Berikan penilaian anda tentang kesesuaian pasangan syaf-cakera dengan p emas angan int erfer ens bil a dib andingkan deng an p em as an gan menggunaknn kekunci dan alur kekunci sebagai cara menetapkan cakera kepada syaf apabila menghantar kilas. (20 markslmarknh) -oooooooo-...8/-

IEMM 22u31 LAMPIRAN I Average Mechanical Properties of Typical Engineerine Materials (SI Units) Materials Metallic Density p (Mg/mt) Modulus of Elasticity,E (GPa) Modulus of Rigidity G (GPa) Yield Strength (MPa) Coef. of Therm. Expansion cr, (10-1/"C Aluminum { ZOl4-fe Wrought Alloys L OOOt-te 2.79 2.71 73.1 68.9 )1 26 414 255 23 24 Cost Iron fgray ASTM 20 Alloys LMaileable ASTM A- 197 7.19 7.28 67.0 1.72 27 68 12 t2 Copper,-Red Brass C83400 Alloys fbronze C86100 8.74 8.83 101 103 37 38 70.0 345 18 17 Magnesium Alloy [Am 1004- T6U 1.83 44.7 18 152 26 [-Structural.{36 Steel Alloys -] Stainless 304 ' -ToolL? r Titanium Alloy J [Ti-6A I-4V] 7.85 7.86 8.16 4.43 200 193 200 120 /J /J 75 44 400 517 800 r000 12 t7 t2 9.4 Nonmetallic Concrete ill.ow Strength thigh Strength 2.38 2.38 22.r 29.0 ll ll Plastic <F(evlar 49 Reinforced L30Vo Glass 1.45 1.45 131 72.4 [1/U