Consider the beam shown in (Figure 1). Suppose that 12 kN/m. Figure B ܝܐ 60⁰ 6 m W 1 of 1 60 kN-m

In the figure below, a horizontally-oriented beam is supported by a hinge at point A as well as a cable.  The beam length between points A and B is 20 meters, the distance (m) between the beam end and the cable attachment point is 16 meters.  The height (l) of the cable attachment above the hinge is 15 meters.  The weight attached at point B is 200 Newtons.  The beam is uniform density with a weight of 100 Newtons.  Beam weight can be assumed to apply at the beam mid-point.    How many unknown forces and/or moments are present?   Group of answer choices 0 1 2 3

n the figure below, a horizontally-oriented beam is supported by a hinge at point A as well as a cable.  The beam length between points A and B is 20 meters, the distance (m) between the beam end and the cable attachment point is 16 meters.  The height (l) of the cable attachment above the hinge is 15 meters.  The weight attached at point B is 200 Newtons.  The beam is uniform density with a weight of 100 Newtons.  Beam weight can be assumed to apply at the beam mid-point.    The beam is statically determinant - true or false? Group of answer choices True False

A 4-meter cantilever beam supports a uniformly distributed load of w=25 kN/m at half of its span; located at 2 m. The beam is I-shaped, in cross-section and has the dimensions as shown in the attached image. Here, EI is constant for the beam. Please help me in determining the following; (a) What are the Bending Moment and Shear Force Diagram for this beam? (b) What is the geometric centroid and moment of inertia of the I-beam cross-section? (c) What is the magnitude and location of the maximum bending stress within the beam?Thank you in advance for your help :)

The figure shows a cantilever of length L= 4 m consisting of steel angles size of 100 x 100 × 12 mm mounted back to back. The cantilever is subjected to a point load P= 1500 N acting at a = 2.5 m and a distributed load w= 1100 N-m-. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. P a В Find the deflection at B. The deflection at B is – 4.46 mm.

A steel beam is loaded as shown in the figure. Determine the following by using conjugate beam method: a. Slope at A b. Slope at B c. Displacement at the point of application of the 15kN load d. Displacement at C e. Location and maginitude of maximum deflection

In the figure below, the beam is cantilevered from the wall. The connection of the beam to the wall can be considered a general interaction. The beam has a uniform density, so it will be subject to a weight force applied mid-way between points A and B. length from point A to point B =10.0 meters; weight applied at point B = 1.00 kN; beam weight = 0.500 kN Beam embeded in cwall a cautilever What is the magnitude and direction (relative to the x-y coordinate system shown in the upper left portion of the figure) of the moment applied by the wall support? O 12.5 kNm into the screen O 50.8 kNm out of the screen O 38.5 kNm into the screen O 97.5 kNm out of the screen

analyze the shown beam using: 1- force method 2- stiffness method assume that A is pin support and B is roller support 7kN/m em 11kN B 4 m m

In the figure below, the beam is cantilevered from the wall. The connection of the beam to the wall can be considered a general interaction. The beam has a uniform density, so it will be subject to a weight force applied mid-way between points A and B. length from point A to point B =10.0 meters; weight applied at point B = 1.00 kN; beam weight = 0.500 kN Beam embeded in cwalla cautilever B A What is the magnitude and direction (relative to the x-y coordinate system shown in the upper left portion of the figure) of the horizontal and vertical components of the wall support? horizontal = 0 N, vertical = 1.50 kN O horizontal = 1.50 kN, vertical = 0N O horizonatl = O N, vertical = 1.00 kN O horizontal = ON, verttical = 2.00 kN

per the attached figure: the beam is to be cut longitudinally along both sides as shown. if it is made from a material having an allowable shear stress of Tallow = 80 MPa, dteremine the maximum allowable shear force V that can be applied before and after the cut is made.