assume:
width (mm)= 30
overlap (mm)= 21
glue strength (n/mm^2)= 1
assume: width (mm)= 30 overlap (mm)= 21 glue strength (n/mm^2)= 1 3. See the double lap joint shown below. Assume that...
Assume: width (in)= 2 thickness (in)= 0.25 force (ib)= 500 pin diameter (in)= 0.5 4. See the pin joint shown below, the force, pin diameter width and link thickness from the spreadsheet. Assume the link is made of steel with strength of 36,000 psi and pin shear strength of 21,600 psi. Ignore the ears. a. Is the pin in single or double shear? b. Given the force and pin dimensions, what is the shear stres:s in the pin? c. Given...
Will rate, thank you Assume a plane stress load case for the double lap (double plate) joint for three plates. Plate is sandwiched by Plate 2 and Plate 3. They are joined by a fastener. Assume that Plate 2 and Plate 1 are subjected to axial loads of 10,000 lbs and 12,000 lbs respectively. Furthermore there is an external axial load T of 1000 lbs acting on the fastener The bar has a length of 15 inches, a height of...
Problem 2) Combined Loading (30 points) The structure shown has a diameter of 40 mm. The length dimensions are a 500 mm and d -100 mm. Using load magnitudes of P.-3000 N, 1000 N, and B-1500 N, determine the normal and shear-stresses in the structure at point H. (Point H is co-planar with the x-y plane.) The cross-sectional properties are A 1257 mm2 J = 251,327 mm" 1,-1,-125,664 mm4 emax -5333 mm3 Present your answers in the following stress tensor...
Problem 2) Combined Loading (30 points) The structure shown has a diameter of 40 mm. The length dimensions are a# 500 mm and d-100mm. Using load magnitudes of = 3000 N, 1000 N, and B = 1500 N, determine the normal and shear stresses in the structure at point H. (Point H is co-planar with the xy plane.) 乃 The cross-sectional properties are: A 1257 mm2 251,327 mm l, = 1.-125,664 Ton" Qmax 5333 mm Present your answers in the...
The joint shown in Figure 1 is made from steel Grade 350 (AS/NZS 3678). Four bolts are used. Diameters of all holes are 5 mm. Note that the middle hole on both Plates A is just a hole with no bolt. The shear design capacity (reduced nominal capacity) of the bolts in single shear is 10 kN. Dimensions given below are in mm. Determinre the maximum tension design force: a) * N2PlatesA that the double plate A can support. b)...
3 (15 points) A bent circular cantilever beam of uniform diameter of 25 mm is shown in igure below. The beam is made from a material with elastic modulus is 70 GPa, the tensile strength is 250 MPa, and the ultimate strength is 300 MPa. 250 mm A. 150 mm z Zz. 50N V (z direction) 100 N (a) (5 points) What are the stresses in the beam at point A? (b) (10 points) Based on your calculations in (a),...
Question 1 (30 Marks) Plate A is fillet-welded to Plate B as shown in Figure 1. Plate A and Plate B have the same material properties Both plates are 10 mm thick. There are two holes (with a diameter of d) in Plate A. It is assumed that weld failure will not occur (a) If Plate A has a yield stress (fy) of 350 MPa and an ultimate tensile strength (fu) of 450 MPa, what is the maximum load (P)...
PROBLEM 2: 40% A 6 kN force is exerted on the frame which has the T cross sectio analyze the states of stress at a section taken at 800 mm from the point of n shown below. It is required to 1. For the given T cross section, find the centroid and the area moment of inertia I,. 2. Draw the free body diagram of the free end of the frame and determine the interna loadings at the centroid of...
A 3 m rigid bar AB is supported with a vertical translational spring at A and a pin at B The bar is subjected to a linearly varying distributed load with maximum intensity g Calculate the vertical deformation of the spring if the spring constant is 700 kN/m. (ans: 21.43 mm) 2. A steel cable with a nominal diameter of 25 mm is used in a construction yard to lift a bridge section weighing 38 kN. The cable has an...
need solution for milestones A Q1 Solid Mechanics 3 Assessment Task 1a - 2020 Milestone a Question 1. For each of the plane-stress conditions given below, construct a Mohr's circle of stress, find the principal stresses and the orientation of the principal axes relative to the xy axes and determine the stresses on an element, rotated in the x-y plane 60° counterclockwise from its original position: (a) dx = 200 MPa Oy - 300 MPa T .40 MPa (b) dx...