h |C b.

Q: 1- The simply supported beam in figure below has a rectangular cross section 120 mm wide and 200 mm…

A:

Q: Question 1) F=36 kN single load, M=48 kN.m moment and w=20 kN/m distributed load act on the beam…

A:

Q: A ec=K L B b→,K 1. (Section)

A:

Q: Question 1) F=16 kN single load, M=22 kN.m moment and w=11 kN/m distributed load are acting on the…

A: As per the guidelines we will answer the first three subparts for you. for the rest of the subparts…

Q: Two uniformly distributed loads of w = 3300 lb/ft act on the simply supported beam shown in Figure…

A: A moment of inertia is the mass of the body when the body is rotating on an axis (resisting any…

Q: Consider the beam shown in (Figure 1). Suppose that w1 = 460 N/m , w2 = 230 N/m . Follow the sign…

A:

Q: Question 1) F=35 kN single load, M=45 kN.m moment and w=16 kN/m distributed load are acting on the…

A: A pin support will exert both horizontal and vertical components of reaction. The support A is pin…

Q: Consider the beam shown in the figure. The allowable tensile and compressive of a beam material are…

A:

Q: F=16 kN single load, M=22 kN.m moment and w=11 kN/m distributed load are acting on the beam whose…

A: Given data, The inclined applied force, F = 16000 N The applied moment, M = 22000 Nm The applied…

Q: If w = 25 kN/m., calculate the value of EIδ at 1 m. of the free end of the loaded beam as indicated…

A:

Q: In the figure, find the length c of the overhangs so that the beam made of U profile can carry the…

A: Permissible stress is stress which produces due to pressure or forces which does not exceed the…

Q: The cantilever beam shown is subjected to a concentrated load of P-70800 lb. The cross-sectional…

A:

Q: Use Castigliano's theorem to compute vertical and horizontal displacements at the point of…

A: Given data,

Q: Example 4: Determine Aa, and Os for the statically determinate cantilever beam. Use 750 x 800 square…

A: A beam gets deflected by applying an external load over it. There are mainly three types of beams,…

Q: A T beam supports the three concentrated loads shown in the figure. If load P=1470 lb is applied on…

A:

Q: 4. A cantilever beam with cross section shown below and span of 3 m is subjected to concentrated…

A: Given Data: The span of the beam is L = 3 m. The concentrated load acting on the beam is P at its…

Q: Q-5. Calculate the maximum allowable internal bending moment M that can be applied to the beam. The…

A: The given figure is symmetrical, and thus the centroid will lie at the mid of the section. The…

Q: Consider the fiberglass beam shown in (Figure 1). Suppose that w1 = 4.6 kN/m and w2 = 5.1 kN/m.…

A:

Q: Find the y coordinates of points H and K. Yu = i mm YK = i mm Save for Later Using multiple attempts…

A:

Q: A flanged wooden shape is used to support the loads shown on the beam. The dimensions of the shape…

A: The load at C, Pc = 1850 lbThe load at E, Pe = 2160 lbThe intensity of UDL, w = 830 lb/ft

Q: A flanged wooden shape is used to support the loads shown on the beam. The dimensions of the shape…

A:

Q: Calculate the value of El6 at the center of the supports of the beam in the following figure: 120 kN…

A:

Q: Question 1) F=35 kN single load, M=45 kN.m moment and w=16 kN/m distributed load are acting on the…

A:

Q: A uniformly distributed load of 200 lb/ft is carried on a simply supported span. If the cross…

A:

Q: Since the safety normal stress of the wood used for the beam and loading condition shown in the…

A: Safety normal stress, σmax=12 MPa=12*103 kPa

Q: 2. The cantilever beam shown in the figure below is subjected to loads P, = 3 kips and P, = 8.5…

A:

Q: The simply supported beam shown in Figure 1 (see next slide) spans a distance of L = 6 m and carries…

A: Given data: L=6 mma=1.5 mb=30 mmd=240 mmt=9.5 mmd=240 mmThe modulie of elasticityof wood planks is…

Q: 3. An aircraft floor beam is made of a 100" length of extruded aluminum with Ftu=76 ksi, Fsu=60 ksi,…

A: Maximum shear stress in the section . ∵t1≠t3    t1=t2 and W1=W2    T=220 in-lb CCW    h'=h-t12-t22…

Forming and Shaping

Metal forming is a category of metalworking process through which the material can be given the desired shape and size by subjecting it to plastic deformation, where the component undergoes bulk deformation process upon application of loads. Unlike the shearing and machining process, the material does not undergo up to a failure point as indicated in the stress-strain curve. Hence, the stresses induced during the forming process are greater than yield strength but less than the failure strength of the material. The process does not lead to the loss of material, so it can be said to be an economical process. During forming, the material is subjected to tensile forces, compressive forces, bending, and shearing loading conditions. The material should possess the property of ductility to undergo the forming process.