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2) For the showing figure, it is required: 4t - To find and draw normal stress...
the steel lever shown in figure
is loaded by a vertical force f=2000 N. A stress element is located
on the upper side of the lever at A (on the smaller diameter) as
shown .Draw the stress element at A showing the magnitude and
directions of the stresses acting on it and find the principal
stresses and directions.
Problem 3 The steel lever shown in figure is loaded by a vertical force F = 2000 N A stress element is...
Find the normal U a. b. Find the maximum shear stress and plltip c. Find the safety factor using the distortion-energy (Von MiSe Problem 2 [20]: A simply supported shaft with overhanging load is shown in Figure 2 force P is applied as the shaft rotates. The shaft is also subject to a constant torque of T ignoring Tmin, find the diameter of shaft required to obtain a safety factor o shaft is steel of Sut - 118 kpsi and...
The member shown above has a W - shape cross séction. FINDa) draw the shear, moment and normal force diagramb) determine the absolute maximum bending stress in the beam and
draw the stress distribution over the cross section at this
location.c) draw the transverse shear stress distribution over the cross
section just to the right of point B.d) determine the state of stress that the loading produces at
point E and point F.e) Draw mohr's circle for state of stress at...
3. Figure shows a state of plane stress consists of normal stresses 60 MPa and Ly-40MPa; and unknown shear stress, The maximum principal stress was determined to be 104.34 MPa. Using Mohr's cirdle, determine a. the magnitude of the shear stress, b. the principal plane and the minimum principal stress. Then, sketch the element showing all stresses in its proper orientation, c. the maximum shear stress, associated normal stress and the orientation of the element. Then, sketch the element showing...
2) Draw two schematic graphs using pencil showing a typical stress-strain curve for aluminum. The first graph should show engineering stress vs engineering strain, and the second graph should show true stress vs true strain. Label the showing: (i) elastic modulus (ii) proportional limit (iii) yield stress (iv) yield strain (v) fracture stress (vi) fracture strain on each graph. You may show both graphs on one plot. (5 points)
Convert cross section into complete steel
Find normal stress at point of interest
Find shear stress at point of interest
Not
imcomplete. The bottom figure shows beam under loading. Upper
figure shows cross section. So, shear and moment diagrams must be
sketch first then you can proceed with normal & shear
stresses.
Steel 11 Stee WOOD Es = 30 3 kip/ 3 kip/ 5 kip-It
2) Given the stress shown on the figure below: 8 MPa 3 MPa - - 5 MPa 3 MPа Note that this plot is not to scale Required: a. Evaluate Oa and Ta when a = 25° b. Evaluate o, and 03 c. Find the maximum shear stress and the orientation of the plane in which it acts. d. Found the normal stress associated with the maximum shear stress
a. Find the curvature of the curve r(t)- (9+3cos 4t)i-(6+sin 4t)j+10k. o. Find the unit tangent vector T and the principal normal vector N to the curve -π/2<t<π/2. r(t) = (4 + t)i-(8+In(sect))j-9k, Find the tangential and normal components of the acceleration for the curve r(t)-(t2-5)i + (21-3)j +3k.
a. Find the curvature of the curve r(t)- (9+3cos 4t)i-(6+sin 4t)j+10k. o. Find the unit tangent vector T and the principal normal vector N to the curve -π/2
Problem 1 (27 points) Consider composite beam shown in image below. a) Draw internal force diagrams (6) b) Draw transform section and find its moment of inertia (9) c) Draw normal stress and strain diagram at cross-section with max moment (6) d) Find shear stress at the interface between PVC and Escon (6) 500 lb 500 lb PVC Epvc 450 ksi Escon EF160 ksi 3 ft 3 ft in. 2 in 3 in.
Problem 1 (27 points) Consider composite beam...
Question 5 a) Determine the normal stress and shear stress acting on the inclined plane AB as shown in Figure 7. Solve the problem using the stress transformation equations. Show the result on the sectioned element. B 45 MPa 80 MPa 45° Figure 7 [4 marks) Determine the principal stress, the maximum in-plane shear stress, and average normal stress for Figure 8. Specify the orientation of the element in each case. b) 200 MPa 500 MPa 350 MPa Figure 8