USE IMAGE BELOW Question; Draw and fully label the Freebody diagram of the BEAM in the picture below.

A uniform beam is fixed at end x=0 and simply supported at x = L. Find the shape of the center line of the beam, given the weight per unit Length is w. a. b. C. e. O y(x) = d. y(x) = a y(x) = y(x) = y(x) = W 24 El -[x4 - 4Lx³ +6L²x²] =[x4-2Lx³ + L²x²] -[x4-2Lx³ + L³x] -[2x4-5Lx³+3L²x²] [2x4-3L³x³ +3L²x²] W 24 El W 24 El W 24 El - W 24 EI

The beam is subjected to a point load and a distribution load as shown in Figure 2-1 below.(a) Draw a Shear Force Diagram in the beam ABC interval.(b) Draw a Moment Diagram in the beam ABC interval.(c) If the cross-sectional area is shown in Figure 2-2, how many mm is the neural axis NA from the bottom?(d) Find the second moment of area, INA from the natural axis.(e) Find the maximum shear stress JJ on the stem side at the connection between flange and stem in the beam ABC interval. (f) Find the maximum shear stress mmax in the beam ABC interval.(g) Find the maximum tensile flexural stress mmax, T and maximum compressive flexural stress mmax, C in the beam ABC interval, respectively.

For the composite beam section in Figure Q2b, calculate the second moment of area (Ixx) about its centroid x-axis.

Draw (FBD) and calculate the support reactions in the simply support beam ABCD below 0.3m B 3kN 0.5m 1.2m 5kN Lo ** 60⁰ 0.4m

Subject  :- mechanical engineering

For each of the beams below draw the FBD, V diagram, and M diagram.

Pin-joint construction supports point loads as shown below: P Al ΕΙ C B 2/3 L 1/3 L a) Find the equation for the deflection of the bar at point B! b) Determine the equation for the moment that occurs at point A!

For the structural beam loaded and supported as shown in Figure 2, (a) Draw a free body diagram and find the support reaction forces/moments.

1. In figure (1), shows a uniform beam subjected to a linear increasing distributed load. The equation for the resulting elastic curve is: w y = 120EIL (-x5+2L?x3 - L*x) Using the numerical methods to determine the point of max. deflection (that is, the value of x where "Y 0. Then substitute dx this value in the given equation to find the value of maximum deflection. Using the following parameter values in your computations: L = 600cm; E50000 k N/cm2;1=30000cm* and w =2.5k N/cm. (a) r Ly 0) =0, v- 0) (b) Figure (1)