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b(mm)=60 d(mm)= 90 P(kN)= 50 e1=(mm) =15 A B Q 2. Determine the resultant stress at...
Y b = 60 m a = 50 mm D н| P = 15 KN B X 2 P2 = 18 KN Figure (13) 161- For problem Figure (13), at the transverse section of member contains the Points H and K, The value of the normal force is a) -15 kN. b) + 15 kN. c) - 18 kN. d) + 18 kN. 162- For problem Figure (13), at the transverse section of member contains the Points H and K,...
Only information given e QUESTION 4 The T-section short column shown in Figure 4 carries an eccentric load P of 100 kN at the position indicated. Determine: (13 The stress induced at the location of the load P; 4.1 4.2 The stress induced at location A, and; 4.3 The position of the neutral axis. 100 mm E X 40 mm Figure 2. T-Section short column. e QUESTION 4 The T-section short column shown in Figure 4 carries an eccentric load...
A rectangular beam is subjected to the loadings shown in Figure Q.16(a) has cross section of 100 mm x 300 mm as shown in Figure Q.16(b). An axial load of 5 kN is applied along the centroid of the cross-section at one end of the beam. Compute the normal stress and shear stress at point P through the cut-section of P in the beam. [15 marks] у 10 kN/m P Ž 5 KN --- 00 P k 3 m -...
3) (40 pts) The EXTERNAL 35 kN force P is applied to the end of a 2 m long cantilever beam with the given cross section. The force acts through the shear center, forming an angle of 35 with the horizontal axis. The x, y axes pass through the centroid C. The y-axis can be assumed to coincide with the right- hand edge of the vertical section. Determine (a) the normal bending stress at Point A, (b) normal bending stress...
A cantilever beam, with a rectangular cross section, is subjected to loads P, Q and R, as illustrated in the figure below. Given, P 100 kN, Q 15 kN and R 10 kN, determine the principal stresses and the maximum in-plane shearing stress at point B. Also, determine the planes on which the principal stresses act, and the planes on which the maximum in-plane shear stress acts. The vertical dimension (depth) of the beam is 120 mm. 40 mmA 2...
M8.16 The transformed-section method scenes 210 mm 28 mm E 160 GPa E=90 GPa 76 mm K 240 mm y (mm) A composite beam cross section consists of two rectangular bars securely bonded together. The beam is subjected to a bending moment M = 20 kN-m that produces compression stress at H Determine: Oн (MPa) a) the vertical distance from K to the horizontal centroidal axis Ок (MPa) b) the bending stress produced at H c) the bending stress produced...
L1(m)=1.5. L2(m)=1.5. w(kN/m)=3. P(kN)=10. M(kNm)= 8. B(mm)= 12. D(mm)=18 Q 4. Draw SFD and BMD for the beam given below and determine the absolute maximum bending stress in the beam if it has a rectangular cross-section of width (B) and depth (D). [7 marks) w kN/m PKN M kNm A B E 4 22 L1 L2 L2
The horizontal force of P = 90 kN acts at the end of the plate. The plate has a thickness of 10 mm and Pacts along the centerline of this thickness such that d = 50 mm. The position of P is shown with a red spot on the centerline in a side view. a) Determine normal stress at point A (10 points). b) Determine normal stress at point B (10 points). c) Plot the distribution of normal stress acting...
A circular column segment, shown in Figure 2, is subjected to a concentric 1,000 kN compression force, and 100 kNm torsional forces. For this column segment: a Calculate the normal stress at point A, due to the axial load b) Calculate the shear stress at point A, due to the applied torque c Determine the major and minor principal stresses, the maximum shear stress, and the angle to the principal axes at point A. d) Draw a diagram illustrating the...
P = 20 kN. Calculate the following: 1. The maximum tensile and compressive stresses at the base of the mast A 2. The maximum tensile and compressive stresses at point B of the mast For each stress state at A and B indicate which side of the mast experiences tension and which side experiences compression. 0.25 m m D w 3 m H С. - 0.1 m mast cross section 3 m 60° Р B 584 mm 6 m mast...