1. Match the following distributed loads with the proper shear and moment diagrams. V w M...
Match the following distributed loads with the proper shear and moment diagrams. B C 3 Me Il . Which of the following trusses have zero force members? A A Which of the following is true for a typical force vector? a. There can be up to 3 rectangular components. b. The resultant of two force vectors can be obtained using the parallelogram law C. A negative value represents direction, while the magnitude is always positive d. All the above The...
1. Match the following distributed loads with the proper shear and moment diagrams. W V A W 1 Shear V R Moment V wa Shear M B 2 X Moment M R R V CRA 3 1 Shear M V Moment V Shear D 4 + Z MA VA R R Moment
3. Which of the following is true for a typical force vector? a. There can be up to 3 rectangular components. b. The resultant of two force vectors can be obtained using the parallelogram law C. A negative value represents direction, while the magnitude is always positive d. All the above ^ 4. The principal moments of inertia represent the minimum and maximum moments of inertia about any ossible axis of a section. a. True / b. False 7
#1) (65p.) Draw the Shear Force (V) and Bending Moment (M) diagrams of statically indeterminate beam shown in figure using “Force Method”. The (roller) support at “B” settles 35 mm. The moment of inertia is given by (1) for regions “AB”, “BC” and “CD”; however it is equal to (21) for the region “DE”. (“B” is the roller and “E” is the fixed type of support). [The flexural rigidity: EI=40000 kNm?] 60 kN 10 kN/m 1 A B X (1)...
For the beam shown in Fig.3, q1= 10kN/m, Mo=15kN.m. a) Find all support reactions. b) Find the expressions for the shear force V and bending moment M. c) Draw the shear-force and bending-moment diagrams. Note that Mo acts at C, and dV/dx = -q, dM/dx = V Calculate (a) the maximum shear stress in each segment; (b) the angles of twist (in d at the mid-span of the larger segment. Given: r-Trllp Ti 91 T: Fig. 2 Fig. 3 q,-10...
For the beam shown in Fig.3, q1= 10kN/m, Mo=15kN.m. a) Find all support reactions. b) Find the expressions for the shear force V and bending moment M. c) Draw the shear-force and bending-moment diagrams. Note that Mo acts at C, and dV/dx = -q, dM/dx = V Calculate (a) the maximum shear stress in each segment; (b) the angles of twist (in d at the mid-span of the larger segment. Given: r-Trllp Ti 91 T: Fig. 2 Fig. 3 q,-10...
#1) (65p.) Draw the Shear Force (V) and Bending Moment (M) diagrams of statically indeterminate beam shown in figure using “Force Method”. The (roller) support at “B” settles 35 mm. The moment of inertia is given by (I) for regions “AB”, “BC” and “CD”; however it is equal to (21) for the region “DE”. (“B” is the roller and “E” is the fixed type of support). [The flexural rigidity: EI=40000 kNm’] 60 KN 10 kN/m A B X (I) (I)...
#1) (65p.) Draw the Shear Force (V) and Bending Moment (M) diagrams of statically indeterminate beam shown in figure using “Force Method”. The (roller) support at “B” settles 35 mm. The moment of inertia is given by (I) for regions “AB”, “BC” and “CD”; however it is equal to (21) for the region “DE”. (“B” is the roller and “E” is the fixed type of support). [The flexural rigidity: EI=40000 kNm’] 60 KN 10 kN/m A B X (I) (I)...
#1) (65p.) Draw the Shear Force (V) and Bending Moment (M) diagrams of statically indeterminate beam shown in figure using “Force Method". The (roller) support at "B" settles 35 mm. The moment of inertia is given by (1) for regions "AB", "BC" and "CD"; however it is equal to (21) for the region "DE". ("B" is the roller and "E" is the fixed type of support). [The flexural rigidity: El-40000 kNm"] 60 KN 10 kN/m B (1) (1) D (21)...
#1) (65p.) Draw the Shear Force (V) and Bending Moment (M) diagrams of statically indeterminate beam shown in figure using "Force Method”. The (roller) support at “B” settles 35 mm. The moment of inertia is given by (I) for regions "AB", "BC" and "CD"; however it is equal to (21) for the region “DE”. (“B” is the roller and “E” is the fixed type of support). [The flexural rigidity: EI=40000 kNm] 60 KN 10 kN/m B (21) 1.5 m 1...