Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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For the beam loaded as shown, determine the reaction components using each of the following methods: 1.)Double Integration Method 2.) Area Moment Method 3.)Conjugate Beam Method4.)Method of Three Moments Use E=200 GPa,I=800x106mm4whennecessary.
Assigned P values 167.5
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- Using double integration method derive an expression for the maximum value of deflection for the simply supported beamarrow_forwardThe simply supported beam shown in Fig. P-610 carries a uniform load of intensity w symmetrically distributed over part of its length. Determine the maximum deflection ô and check your result by letting a = 0 and comparing with the answer to Problem 3. Wo 2b a R1 R2arrow_forward2. A uniform, simply supported beam, is loaded as shown in Figure 2. Using singularity functions, determine an expression for the bending moment at any point along the beam. Hence, determine the slope of the beam at point, A, and the deflection of the beam at point, B. The bending stiffness of the beam is 3200 Nm². 320 N 200 N/m 1.2m 0.6m Figure 2 2 A 0.4m X * B Darrow_forward
- solve step by step in digital format Solve the following exercises by the conjugate beam method A 18 ft 6 klb/ftarrow_forwardUsing double integration method, determine the maximum deflection of the beam shown. (Hint: utilize symmetry, analyze only right half of the beam.) w w В L/2 L/2arrow_forwardSolve q4 a and b both parts plz solve this in maximum one hour if u can't solve this u can reject in half hour so that i can't wait of your answer plz..arrow_forward
- Solve q4 part both parts c ,d and e plz solve this in maximum 2 hour if u can't solve this u can reject in one hour so that i can't wait of your answer plz..arrow_forwardDetermine the internal moments at the supports of the beam shown using: 1.) ThreeMoment equation 2.) Moment Distribution Method 3.) Slope-Deflection Method Pick two method only Given: E=200GPa I=20x10^6 mm^4 w=8kN/m L1=10m L2=8marrow_forwardUsing Double Integration Method derive an expression for the maximum value of deflection for the simply supported beamarrow_forward
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