a) Find minimum diameter nceded if the allowabe shear stress is 140 Mpa and the otation of point A can't exced 2.5 degreas. 10 kN-m 4KN m QUN -m A 900 mm (l goo mm 450 mm
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- Where is/are the location(s) of the maximum transverese shear stress? A simple I-beam is loaded as shown. 20 mm P KN PKN PKN Į Į -C B с D L/4 m L/4 m Midspan at point C Roller at E at the NA Section B at the top fiber Pin A at point C Midspan at point D Roller E at point D L/4 m L/4 m OE 20 mm 20 mm- 250 mm 150 mm 150 mm A8. H / The beam shown below has across seclion of channel Shape with width 360mm.and haghs h= loomm, the web thickness ist= 14mm.Deler- Mine ihe Max imum tensile aud Compressive stressin the beam due to unifom Load? 360Mm 3.6KN/M 14m tiom Please Sir 5T CASIC f-991ES PL DATURAL u CALC (-)I need a clear answer by hand, not by keyboard and fast answer within 20 minutes. Thank you | dybala For the beam loaded as shown, find the maximum tensile and compressive bending stresses and maximum shearing stress.. IN.A=4*10mm* 80mm 100mm 60mm 60mm 1.5KN 2kN/m 1mal A |-----|- | Im ++ Im->> 3m 3kN/m
- 4 Determine the design angle 8 for connecting mem- ber A to the plate if the resultant force is to be directed vertically upward. Also, what is the magnitude of the re- sultant? F₁ = 500 N -00 00 y ooo B FB = 400 N XQ4\ Which of the following is a zero-force member? 3 8KN 4 G 4 エ 子c D. 4 B AC BD IF ID10/10 find the tensile stress in upper plate in section 3-3 80 kN 80 kN 8-bolt DIA. 10 MM 80 kN 80 kN 8-bolt DIA. 10 MM 10 MPа О 12.5 MPa 15 MPa 8.5 MPa O no one O ---.. O- O O 300mm 8 mm
- Acantilever beam AB, loaded by a uniform load (see figure), is applied on a channel section. If the cross section has the dimensions indicated and the moment of inertia about the z axis (the neutral axis) is I= 3.36 in" Find the maximum tensile stress fhtMAX and maximum compressive stress facMAX (Note: Draw the shear and moment diagram). 2.5 lb/ft 0.617 in. Z- C 2.269 in. 6.0 ftEN O Aロa。 USEFUL LINKS v M Time Select the reinforcing needed for the short tied column shown for the following: Pn=2000 kN, 250 mm, e 200 mm. f28 MPa, fy= 420 MPa: (Add attachments below) 70 s00 mm 640mm 70 mm 70 mm 70 mm 210 mm 350 mmTest#1 -zzen-zax AlpQLSdM75VMOVqbMa1WtS9n99RYc6PifeGUTpVBOluyMUUVYQgqqA/formResponse YouTube Replace the three forces which act on the bent bar by a force-couple system at *.the support point A 2100 lb 4' 1500 lb •A B. 30° C. 2' •E. 800 lb 3' oogle
- 10/10 find the tensile stress in upper plate in section 1-1 80 kN 80 kN B-bolt DIA. 10 MM 80 kN 80 kN 8-bolt DIA. 10 MM 30 МРа О 33 МРа О 35 MPа 37 MPa no one 300 mm O- O 4)4 - For the beam loading configuration and cross-section shown below, what is the maximum allowable load P given that the maximum allowable stress (in tension and compression) is 120 MPa? PO Р 1.6m PN ż 0.8m 0.8m P80 1.6m Р 30 30 T 10 dimensions in mm beam cross-section (same as problem 3, but inverted)2. The crank mechanism shown below is in equilibrium. Determine: a) the diameter of cylindrical connecting rod CD, given that normal stress is limited to 120MPa; b) the shear stress in the pin at B, where the pin has diameter of 8mm; and c) the bearing stress in the bracket supports at B. C 120° A 8kN 300mm B 30⁰ D P 200mm 6mm B 15mm 6mm 8mm Detail of pin and pin brackets