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Chapter 12: Static Equilibrium Conditions for equilibrium First condition for equilibrium • When a particle is in equilibrium (no acceleration), in an inertial frame of reference, the vector sum of all the forces acting on the particle is zero. A frame of reference where Newton’s first law is valid F 0 F x 0, Fy 0, Fz 0 The sum includes external forces only. Conditions for equilibrium (cont’d) Second condition for equilibrium • For an extended body to be in equilibrium the body must have no tendency to rotate. L 0 , dL / dt 0 about any point in the body 0 about any point in the body • The sum of the torques due to all external forces acting on the body with respect to any specified point must be zero. • Note that the above conditions apply to a rigid body in uniform translational motion or to constant rotation (if L is constant) as well. But in the following we will mostly consider situations in which a rigid body is at rest, i.e., in a static equilibrium. Center of gravity The center of gravity (= the center of mass) • The gravitational torque about any point can be found by assuming that all the weight of the body acts at its center of gravity Definition of the center of mass • For a collection of particles with masses mi and coordinates xi , yi ,, zi the coordinates of the center of mass are given by: the gravity changes with xcm imi xi / imi Although the altitude, if we can ignore this change, this statement is valid. ycm zcm m y / m m z / m i i i i i i i i rcm imi ri / imi i i The center of gravity coincides with the center of mass when the gravitational field is uniform. Center of gravity (cont’d) Newton’s third law • For a collection of particles with masses mi and the center of mass coordinates xcm , ycm , zcm , Newton’s third law is given by: Fx ,net i f x ,i imi ax ,i ax imi ax M Fy ,net i f y ,i imi a y ,i a y imi a y M Fz ,net i f z ,i imi az ,i az imi az M Fnet Ma ai a For a rigid body M Center of gravity (cont’d) Total torque • Assume that the acceleration due to gravity g has the same magnitude and direction at every point in the body • For a collection of particles with masses mi and coordinates the total torque is given by: ri z y rcm mi ri O cg=cm ? i i iri mi g (imi ri ) g rcm imi rcm M w Mg wi mi g x M rcm Mg rcm w • If g has the same value at all points on a body, its center of gravity is identical to its center of mass How to find and use center of gravity How to find cg • The center of gravity of a homogeneous sphere, cube, circular sheet, or rectangular plate is at its geometric center. • The center of gravity of a right circular cylinder or cone is on its axis of symmetry. • For a body of more complex shape, the center of gravity can be located approximately by dividing the body into symmetrical pieces. • When a body acted on by gravity is supported or suspended at a single point, the center of gravity is always at, or directly above or below the point of suspension because there should not be any torque. • A body supported at several points must have its center of gravity somewhere within the area bounded by the supports. How to find and use center of gravity (cont’d) How to use cg Ex.1 Ex.2 + Ex.3 stable : cg is within the area of support area of support unstable: cg is outside the area of support area of support Stability Classification of stability U(x) dU ( x) 0 dx d 2U ( x) Stable equilibriu m condition : 0 2 dx dU/dx Equilibriu m condition : All positions above are in equilibrium but: 1 Conditionally stable or metastable (weakly stable) 2 Unstable 3 Conditionally stable or metastable (strongly stable) 1 3 2 x Example from Biomechanics W=Fxd D = distance covered by motion Example for biomechanics (Study Example 12.3) A person holds a 50.0N sphere in his hand. The forearm is horizontal. The biceps muscle is attached 3.00 cm from the joint, and the sphere is 35.0cm from the joint. Find the upward force exerted by the biceps on the forearm and the downward force exerted by the upper arm on the forearm and acting at the joint. Neglect the weight of forearm. FB Since the system is in equilibrium, from the translational equilibrium condition F 0 O l mg F F F mg 0 F From the rotational equilibrium condition F 0 F d mg l 0 d x U y B U U B FB d mg l mg l 50.0 35.0 583N FB 3.00 d Force exerted by the upper arm is FU FB mg 583 50.0 533N Thus, the force exerted by the biceps muscle is Examples of objects in equilibrium Example : Walking a horizontal beam Examples of objects in equilibrium Example : Walking a horizontal beam (cont’d) 2nd condition: 0 wB ( L / 2) wM (1.50 m) TL sin( 53) 0 i T 413 N 1st condition: F F x Rx T cos 35.0 0 y R y wB wM T sin 53.0 0 Rx 249 N, Ry 5.70 102 N wB wM L T Exercises 30.0o (a) Problem 1 Find the tension T in each cable and the direction of the force exerted on the strut by the pivot in each of the arrangements in Figs. In each case let w be the weight of the suspended crate full of priceless art objects. The strut is uniform and also has weight w. Solutions (a) TL tan 30.0 wL w( L / 2) w w T (b) L 30.0o (torque=0) w w 45.0o T 2.60w The pivot exerts an upward vertical force of 2w and a horizontal 2.60w so that the magnitude is 3.2w, dir. 37.6o from the horizon. (b) TL sin 15.0 wL sin 45.0 ( w / 2) L sin 45.0 (torque=0) T 4.10w The horizontal force by the pivot on the strut is Tcos30.0o =3.55w & the vertical 2w+Tsin30o=4.05w so that the mag. 5.38w and dir. 48.8o. Problem 2 A uniform ladder of length l and weight mg=50 N rests against a smooth, vertical wall. If the coefficient of static friction between the ladder and the ground is ms=0.40, find the minimum angle qmin at which the ladder does not slip. First the translational P equilibrium, using components l FBD q n O F F mg f Thus, the normal force is x f P 0 y mg n 0 n mg 50 N The maximum static friction force f smax m s n 0.4 50N 20N P just before slipping is, therefore, From the rotational equilibrium O l mg cosq min Pl sin q min 0 2 mg 1 50 N tan 51 40 N 2P q min tan 1 Problem 3 Three vertical forces act on an airplane when it is flying at a constant altitude and with a constant velocity. These are the weight of the airplane, aerodynamic force on the wing of the airplane, an aerodynamic force on the airplane’s horizontal tail. For a particular light airplane with weight of 6,700 N, the center of gravity is 0.30 m in front of the point where the wing’s vertical aerodynamic force acts and 3.66 m in front of the point where the tail’s vertical aerodynamic force acts. Determine the magnitude and direction of each of the two vertical aerodynamic forces. Fwing Solution .3 m Ftail F 0 : 0 : Ftail W Fwing 0 3.66 m (3.66 m) Ftail (0.3 m) Fwing 0 Fwing 7,300 N (up ), Ftail 600 N (down) w Problem 4 You are trying to raise a bicycle wheel of mass m and radius R up over a curb of height h. To do this you apply a horizontal force F. What is the least magnitude of the force F that will succeed in raising the wheel onto the curb when the force is applied (a) at the center of the wheel? (b) at the top of the wheel? R (c) In which case is less force required? (a) Perp. distance from mg to the upper corner : Perp. distance from F to the upper corner : R 2 ( R h )2 2 Rh h 2 Rh mg 2 Rh h 2 F ( R h) F mg (b) torque by mg = torque by F h mg Solutions torque by mg = torque by F F 2 Rh h 2 Rh mg 2 Rh h 2 F (2 R h) 2 Rh h 2 F mg 2R h (c) Less force is required when the force is applied to the top of the wheel. Problem 5 Max. overhang at L/2 (a) max. overhang? (b) max. overhang? max.overhang Solutions (a) The center of gravity of the top block can be as far out as the edge of the lower block. The center of gravity then is at the mid point between the center of the top and bottom block. The combined center L/4 3L/4 of gravity is at the edge of the table. xmg-(L/2-x)mg=0 for bottom block x=L/4 mg mg x Problem 5 Solutions Answer to part (a) (b) Repeating the argument above the max. overhang for three stacked block is (3L/4)+(L/6)=11L/12. xmg-(L/2-x)2mg=0 for bottom block x=L/3L/2-L/3=L/6 L/4 3L/4 mg 2mg x