please answer with a complete solution O C. 233.2 lbD. 234.3 lbOption 522. the horizontal component at the pin C. *A. 628.6 lbB. 627.8 lbO C. 634.4 lbD. 652.3 lb23. the vertical component at the pin C. *O A. 1468 lbB. 1485 lbC. 1500 lbOD. 1526 lb1 point1 point For nos. 21-23, satisfy the conditions of the given problem below: As an airplane'sbrakes are applied, the nose wheel exerts two forces on the end of the landinggearas shown in the figure 1. Determine:21. the force in the strut AB. *1 pointB-20%1350 lbO A. 215.3 lbB. 224.4 lbA30°450 lb.1 ft2 ft

For nos. 21-23, satisfy the conditions of the given problem below: As an airplane's brakes are applied, the nose wheel exerts two forces on the end of the landing gear as shown in the figure 1. Determine: 21. the force in the strut AB. * 1 point B -20% 30° 450 lb. 1 ft 2 ft

For nos. 21-23, satisfy the conditions of the given problem below: As an airplane's brakes are applied, the nose wheel exerts two forces on the end of the landing gear as shown in the figure 1. Determine: 21. the force in the strut AB. * 1 point B -20% 30° 450 lb. 1 ft 2 ft

Principles of Physics: A Calculus-Based Text

5th Edition

ISBN:9781133104261

Author:Raymond A. Serway, John W. Jewett

Publisher:Raymond A. Serway, John W. Jewett

Chapter10: Rotational Motion

Section: Chapter Questions

Problem 33P: A 15.0-m uniform ladder weighing 500 N rests against a frictionless wall. The ladder makes a 60.0...

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Concept explainers

Rotational Equilibrium And Rotational Dynamics

In physics, the state of balance between the forces and the dynamics of motion is called the equilibrium state. The balance between various forces acting on a system in a rotational motion is called rotational equilibrium or rotational dynamics.

Equilibrium of Forces

The tension created on one body during push or pull is known as force.

Question

please answer with a complete solution

O C. 233.2 lb
D. 234.3 lb
Option 5
22. the horizontal component at the pin C. *
A. 628.6 lb
B. 627.8 lb
O C. 634.4 lb
D. 652.3 lb
23. the vertical component at the pin C. *
O A. 1468 lb
B. 1485 lb
C. 1500 lb
OD. 1526 lb
1 point
1 point

For nos. 21-23, satisfy the conditions of the given problem below: As an airplane's
brakes are applied, the nose wheel exerts two forces on the end of the landing
gear
as shown in the figure 1. Determine:
21. the force in the strut AB. *
1 point
B
-20%
1350 lb
O A. 215.3 lb
B. 224.4 lb
A
30°
450 lb.
1 ft
2 ft

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