If the applied force P causes the point B on the rigid arm ABC to be displaced 0.25 mm downward, determine the normal strain developed in wires BD and CE.
Since ABC is a rigid bar, it does not deform under the action of load. Instead, it merely rotates about A. The displacement of points B and C vertically downwards can be determined by applying similarity of triangles.
If the applied force P causes the point B on the rigid arm ABC to be displaced 0.25 mm downward
The rigid beam is supported by a pin at A and wires BD and CE. If the load P on the beam causes the support B to be displaced 5 mm downward determine the normal strain developed in wires CE and 4m BD.
The rigid beam is supported by a pin at A and wires BD and CE. If the load P on the beam causes the end C to be displaced 10 mm downward, determine the normal strain developed in wires CE and BD.
Question 4 The rigid beam is supported by a pin at A and wires BD and CE. If the load P on the beam causes the end C to be displaced 8 mm downward, determine the normal strain developed in wires CE and BD.
Mechanics of material Question (Problem 2) The rigid beam ABC is supported by a pin at A and wires AB and CE. If the load P acting on the beam causes the end C to be displaced by 15 mm downward, determine the straub developed in wires CE and BD. Also, calculate the load P and the load carried by each wire if wire-200 GPa, dwire-0.1m. 2 m 3 m nm
The rigid bar ABC is supported by a pin at point A and by two wires attached at B and C as shown in the figure. If the applied point load P produces a clockwise rotation of the rigid bar ABC of 5°, find the normal strain for both wires. All dimensions in mm.
If a force is applied to the end B of the member and causes a normal strain in the cable of 0.00367 mm/mm, determine the displacement of point B. Part of a control linkage for an airplane consists of a rigid member CB and a flexible cable AB. e- 800 mm 600 mm Originally the cable is unstretched
Part A If a force is applied to the end B of the member and causes a normal strain in the cable of 0.00478 mm/mm, determine the displacement of point B. Problem 2.15 Part of a control linkage for an airplane consists of a rigid member CB and a flexible cable AB 800 mm 600 mm Originally the cable is unstretched.
2-9. If a horizontal load applied to the bar AC causes point A to be displaced to the right by an amount AL, determine the normal strain in the wire AB. Originally, 0 45 Probs. 2-8/9
If a horizontal load applied to the bar AC causes point A to be displaced to the right by an amount A L, determine the normal strain in the wire AB. Originally, theta = 45 degree.
Express your answer using three significant figures. Review VAEc ? The force applied at the handle of the rigid lever causes the of le The wires are unstretched when the lever is in the 2.4 horizontal position. (Figure 1) (CAHA mm/mm Request Answer Submit Part B wire CG. Determine the average normal strain developed Express your answer using three significant figures. vec AE ww (eccg mm/mm Request Answer Submit Figure 1 of 1 Part C wire DF. Determine the average...