(1) Solve for the moment diagram for the following structure. Choose the redundant as (a) the...
please solve this for me urgently! thank you Draw the moment diagram for the beam shown below. Supports B, C,a respectively. nd o settle 5/8", 1.5", and 0.75" EI-constant E 29,000 ksi 1-7,800 in 20 ft 20 ft 20 ft Draw the moment diagram for the beam shown below. Supports B, C,a respectively. nd o settle 5/8", 1.5", and 0.75" EI-constant E 29,000 ksi 1-7,800 in 20 ft 20 ft 20 ft
Using V = 175 kip and H = 3 kip, draw the bending moment diagram for the frame. To solve for the support reactions, use the force method on the statically indeterminate frame. L-120 in E-29,000 ksi σ-50 ksi Columns: W12x40Ar I 307 in'Z-57.0 in* Girder: W8x31Ar 9.12 in2 Ir 110 in Zx 30.4 in L-120 in E-29,000 ksi σ-50 ksi Columns: W12x40Ar I 307 in'Z-57.0 in* Girder: W8x31Ar 9.12 in2 Ir 110 in Zx 30.4 in
can you show the equations to figure out shear and moment diagram please 25 kip 10 kip 5 kip-ft 1.5 kiplet 1.5 kipfft 7 kip-ft A. AX B C oft 8ft 8ft Callow = 24 ksi Callow = 14.5 ksi (bending + shear) 1. Select an appropriate I shape that will carry the looding. 2. Make Smax < Sallowla 240) sure maximum deflection LAC=16ft both must hint (20=8ft be checked! Note: Your design must satisfy both strength and deflection requirements
Find all forces and draw a shear and moment diagram. 10 kip 25 kip 1.5 kip/ft 1-5 kiple 5 kip-ft 7 kip-ft A B са 8ft eft 8ft A Tallow= 24 ksi Callow = 14.5 ksi >(bending + shear)
solve this using AREA MOMENT METHOD ONLY. show the moment diagram by parts as well Determine the the difference in deflection between the two internal hinges. E 29x103 ksi, I-20in4 Provide complete solutions. 10 k/ft D Hinge 7ft 2 ft 2ft 2ft 21
Provide: a) moment diagram for the primary structure for the applied loads b) moment diagrams for the primary structure for each virtual load used to find flexibility coefficients c) a table indicating the segments you would use and the limits of each (you do not need to write M and m equations) d) setup equations to solve for displacements and flexibility coefficients (you do not need to find them though) e) compatibility equations used to solve for the reactions. In...
P1 P2 А B a b Moment of Inertia 1=11 Moment of Inertia 2=12 For the Beam Shown: Use the DOUBLE INTEGRAL METHOD to determine the deflection at end in inches. For downward deflection enter a negative value. a-11 ft b5ft Moment of inertia 1-11-1.739 in Moment of Inertia 2-12-2,569 in P1=27kip P2=29 kip E 29,000 ksi
Choose the best answers 3 ft, and diameters of 1/8 in. and respectively. These wires are made of a material that has the approximate stress-strain diagram as sho The 1.0-kip load is placed on the platform. The wires AB and AC have original lengths of 2 ft and σ (ksi) 3 ft 80 58 2 ft 0.002 0.01 Internal stress in AB (a) 42.2 ksi (b) 26.5 ksi (c) 50.6 ksi d)31.8 ksi Elastic modulus of the wire material (a)...
Force method for composite structure: Determine the degree of static indeterminacy for the structure and use the force method to find the forces in the steel rods. Draw the shear and bending moments diagram for the wood flexural member. A= roller support C= pin support Force Method for Composite Structure. Determine the 'Degree of Static Indeterminacy (SI)' for the structure shown in Figure 1 and use the force method to find the forces in the steel rods. Also, draw the...
Draw the moment diagram for the beam. Begin by placing the lines of discontinuity. Place the appropriate function between the lines of discontinuity, ensuring the endpoints have the correct values Note-Make sure you place only one vertical line at places that require a vertical line. If you inadvertently place two vertical lines at the same place, it will appear visually correct because the lines overlap, but the system will mark it wrong. add vertical line off delete +add segment ?reset...