F6-15. Determine the maximum stress in the beam's cross section. brus d mot A zibosqqA i bonilob s sinani D 100 mm 30° 75 N m B C 150 mm -y A Prob. F6–15
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- D. C Dx 2 m A G aF E E, 100 N 2 m 2 m 2 m Determine the forces in member FBC of the .truss اخترأحد الخيارات а. 300 b. 100 С. 80 d. 2002-6. Resolve the force F, into components acting along Resolve the force F, into components acting along the u and v axes and determine the magnitudes of the the pos 2- ts ac S. components. she u and v axes and determine the magnitudesong componentsLンレ c31 5.9a حل القود 70° 30° 45° F= 300 N F2 = 500 Nv Probs. 2-4/5/6ZEA @ P 0:01 * Asiacell Iı. HW 2_Equilibrium.p.. HW Determine the resultant force at pins A, B, and C on the threc-mcmber framc. 2m 800 N 200 N/m 2 m H.W. Determine the horizontal and vertical components of force at pins A and D. D. 2m 03 m -1.5m- -1.5 m- 12 kN
- The rigid beam is supported by a pin support at A and steel wires BD and CE (E-200GPA). The steel wires are 1cm in diameter. If the load P is 5kN and the weight of the beam is neglected, solve the tension at wire CE. D. E 4 m +2m- 3 m 2 m O 3.18KN O 3.02kN O 2.87k O 2.73KN O o C3m •Analyze the simple truss shown. H 3 6KN 4m рат жёт C 7KN + 4m W 8KN 4 AM t 4.5m. A Simply Supported Concete beam havig a width of so rn and an effectire hepth g s2oma carries a load includmg its Wergth Wq= 7 kNm and a loncortated loád Pa: 370KN unforaly distributed fectret acting 2m from Peft Support. fi = 207 Apa, fo: 415 Mpa I det the Max factored Shear force. at the Cntical Seetion. 2 det the Spaang of the lo'mm o belween. A to B s det. the Spacing the lommd of Sstrirups between B-C. R370KN A B
- 4-99. Replace the force system acting on the beam by an equivalant fo *4-100. Replace the force system acting on the beam by an equivalent force and couple moment at point B. 3 kN 2.5 kN 1.5 kN 30° A В 2 m 4 m *-2 m- Probs. 4-99/1009-8. A standard steel 14 in. Schedule 40 pipe carries, a 650 lb load at the center of a 28 in. span, simply supported. Compute the deflection of the pipe at the load. 9-8 O-.055in O-.0057in O-032in -.054inE=207GA CROSS-SEcnON OF BEAM 12kN/m 4ocN Poisson's rafio:a3 OKN A 10. 36 KN S1-37 kN 14.27KN O- Im 1) FINO DETERMINACY DEGREE. OF THE BEAM THE 2)IDENTIFY THE POSITION OF THE BEAM ARISES. WHERE THE MAXIMUM BENDING MOMENT MAXIMUN TENS ILE FROM THIS POSITION , CALCLILATE THE COMPRESS VE STRESS , THE CURVATURE, STRESS, MAXIMLIM TENSILE STRAIN AND MAXIMLIM COMPRESSIUE MAYIMU STRAINI.
- 12-13. Determine the shear stress at paint B an the web of the cantilevered strut at section a-a. 2kN 4 kN -250 mm -250 mm- -300 mm- 20 mm 70수m 20 imm S0 mmA.) CREATE A SHEAR DIAGRAM BY AREA MOMENT AND BY PARTS B.) CREATE A M/EI DIAGRAM BY AREA MOMENT AND BY PARTS ITEM 1.0 180 kN 15 kN/m A В C- D -5 m- -5 m- -4 m- El = constant E = 70 GPa %3D I = 2,340 (10°) mm4 %3DBy the con ju g a te -beam m ethod ca lcu la te the slope and de fle ction at the free end C of the overhanging beam ABC. Indic a te the d irection of ro ta tio n (clockw is e or counterclo ckw is e ) and de flection (upward or downward). A Iso calcu la te the defle ctio n at 2 po int D (in d ic a te the direction) and s lo pes e, and en. E = 30 000 k/in andI = 200 in . A a B а + b SUMMAR IZE YOUR ANSWERS (DO NOTROUND OFF INCLUDE ALL DEC IMALS) Required V a lu es Answer U n its D ire ctio n radians ??? S lo pe ec De fle ction AC in ch ??? radians ??? S lo pe 0A S lo pe eB radians ??? De flectio n AD in ch ??? DATA a w ft ft kip ft k/ft 12.0 12.0 13.5 5.8 1.83