Abstract
Friction (from Latin fricare, to rub), is the term given to the resistance caused by the moving of the surfaces of bodies over each other.
Access provided by Autonomous University of Puebla. Download chapter PDF
Similar content being viewed by others
Keywords
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.
5.1 Introduction
Friction (from Latin fricare, to rub), is the term given to the resistance caused by the moving of the surfaces of bodies over each other. The resistance is due to the roughness of the surfaces. The first experiments on friction were made by Guillaume Amontons (1699) when he published his rediscovery of the laws of friction first presented by Leonardo da Vinci. Leonardo da Vinci (1452–1519) studied screws, gears, mechanisms, wear, bearings, friction, and lubrication. At Rochefort in 1781, Charles-Augustin de Coulomb verified the laws friction. The laws of dry friction are: 1. friction is directly proportional to the normal force between the surfaces of contact (Amontons 1st Law); 2. friction is independent of the apparent area of contact (Amontons 2nd Law); 3. friction is independent of the velocity with which the surfaces slide one on the other (Coulomb’s Law). Arthur Jules Morin confirmed and extended Coulomb’s work on friction (1830–1834). He build an experimental apparatus under the supervision of Jean-Victor Poncelet. He developed an apparatus to study the laws of falling bodies presented an accurate experimental proof of Galileo’s result that distances travelled by a falling body increase as the square of the time.
If a body rests on an incline plane, the friction force exerted on it by the surface prevents it from sliding down the incline. The question is, what is the steepest incline on which the body can rest?
A body is placed on a horizontal surface. The body is pushed with a small horizontal force \(F\). If the force \(F\) is sufficiently small, the body does not move.
Figure 5.1 shows the free-body diagram of the body, where the force \(W\) is the weight force of the body, and \(N\) is the normal force exerted by the surface on the body. The force \(F\) is the horizontal force, and \(F_f\) is the friction force exerted by the surface. Friction force arises in part from the interactions of the roughness, or asperities, of the contacting surfaces. The body is in equilibrium and \(F_f=F\).
The force \(F\) is slowly increased. As long as the body remains in equilibrium, the friction force \(F_f\) must increase correspondingly, since it equals the force \(F\). The body slips on the surface. The friction force, after reaching the maximum value, cannot maintain the body in equilibrium. The force applied to keep the body moving on the surface is smaller than the force required to cause it to slip. Why more force is required to start the body sliding on a surface than to keep it sliding is explained in part by the necessity to break the asperities of the contacting surfaces before sliding can begin.
The theory of dry friction, or Coulomb friction, predicts:
-
the maximum friction forces that can be exerted by dry, contacting surfaces that are stationary relative to each other;
-
the friction forces exerted by the surfaces when they are in relative motion, or sliding.
5.2 Static Coefficient of Friction
The magnitude of the maximum friction force, \(F_f\), that can be exerted between two plane dry surfaces in contact is
where \(\mu _s\) is a constant, the static coefficient of friction, and \(N\) is the normal component of the contact force between the surfaces. The value of the static coefficient of friction, \(\mu _s\), depends on:
-
the materials of the contacting surfaces;
-
the conditions of the contacting surfaces namely smoothness and degree of contamination.
Typical values of \(\mu _s\) for various materials are shown in Table 5.1.
Equation (5.1) gives the maximum friction force that the two surfaces can exert without causing it to slip. If the static coefficient of friction \(\mu _s\) between the body and the surface is known, the largest value of \(F\) one can apply to the body without causing it to slip is \(F =F_f = \mu _s N\). Equation (5.1) determines the magnitude of the maximum friction force but not its direction. The friction force resists the impending motion.
5.3 Kinetic Coefficient of Friction
The magnitude of the friction force between two plane dry contacting surfaces that are in motion relative to each other is
where \(\mu _k\) is the kinetic coefficient of friction and \(N\) is the normal force between the surfaces. The value of the kinetic coefficient of friction is generally smaller than the value of the static coefficient of friction, \(\mu _s\).
To keep the body in Fig. 5.1 in uniform motion (sliding on the surface) the force exerted must be \(F=F_f = \mu _k N\). The friction force resists the relative motion, when two surfaces are sliding relative to each other.
The body \(R\!B\) shown in Fig. 5.2a is moving on the fixed surface \(0\).
The direction of motion of \(R\!B\) is the positive axis \(x\). The friction force on the body \(R\!B\) acts in the direction opposite to its motion, and the friction force on the fixed surface is in the opposite direction as shown in Fig. 5.2b.
5.4 Angle of Friction
The angle of friction, \(\theta \), is the angle between the friction force,\({F_f=|\mathbf F}_f|\), and the normal force to the surface \(N=|\mathbf{N}|\), as shown in Fig. 5.3.
The magnitudes of the normal force and friction force, and \(\theta \) are related by
where \(R=|\mathbf{R}|=|\mathbf{N}+ \mathbf{F}_f|\).
The value of the angle of friction when slip is impending is called the static angle of friction, \(\theta _s\),
The value of the angle of friction when the surfaces are sliding relative to each other is called the kinetic angle of friction, \(\theta _k\),
Example 5.1
The prism 1 of mass \(m_1\) makes an angle \(\alpha \) with the horizontal and can slide along the horizontal surface as shown Fig. 5.4. The slider 2 of mass \(m_2\) is prevented from horizontal movement and can slide down on the inclined prism 1. The coefficients of static friction between the prism 1 and the slider 2, between the prism 1 and the horizontal surface 0, between the slider 2 and the vertical support 0 are equal to \(\mu \). The friction is sufficient to prevent the prism from moving without the application of any force.
Determine the greatest value of the horizontal force F that acts on the prism 1 without causing the motion of the system.
For the numerical example use \(m_1= 10\) kg, \(m_2= 5\) kg, \(\alpha = 10^{\circ }\), \(\mu = 0.2\), and \(g=9.81\) m/s\(^2\).
Solution
A reference frame\(xy\) having the \(y\)-axis directed upward and the \(x\)-axis directed along the horizontal surface was considered, as shown Fig. 5.5.
Considering the mechanical system to be the slider-prism combination, the weight of the slider and the external force \(\mathbf{F}\) will act on the prism making the prism to move. In addition to the weights and external force, the mechanical system will also be acted upon reaction and friction forces as shown in Fig. 5.5. The sum of all the forces acting on slider \(2\) can be expressed as:
where \( \mathbf{F}_{02}\) is the of force of the ground (vertical support) on slider 2, \(\mathbf{F}_{02} \perp y-\)axis,\( \mathbf{F}_{f02}\) is the friction force between the ground 0 and slider 2, \( {F}_{f02}=\mu \,{F}_{02}\), \(\mathbf{F}_{12}\) is the force of prism 1 on slider 2, \(\mathbf{F}_{f12}\) is friction force between 1 and 2, \({F}_{f12}=\mu \,{F}_{12}\) and \(\mathbf{G}_{2}\) is the weight of body 2. The frictional force is equal to the product of the static coefficient of friction with the normal force between the bodies in contact. As the direction of the frictional force must resist the tendency to slip. The MATLAB commands for the forces on slider 2 are:
The two scalar equilibrium equations on \(x-\)axis and \(y-\)axis are:
The joint forces reaction forces \({F}_{02}\) and \({F}_{12}\) are
The sum of all the forces acting on the inclined prism 1 can be expressed as
where \( \mathbf{F}_{01}\) is the of force of the ground (vertical support) on wedge 1, \( \mathbf{F}_{f01}\) is the friction force between the ground 0 and 1, \( {F}_{f01}=\mu \,{F}_{01}\), \(\mathbf{F}_{21}=-\mathbf{F}_{12}\) is the force of 2 on 1, \(\mathbf{F}_{f21}=-\mathbf{F}_{f12}\) is friction force between 1 and 2, \(\mathbf{G}_{1}\) is the weight of body 1 and \(\mathbf{F}\) is the horizontal external force on 1. The MATLAB exressions for the forces on prism 1 are:
The equilibrium equations for the prism 1 are:
or
The joint force reaction force \({F}_{01}\) and the external force \({F}\) are:
The numerical results are for the joint forces are:
and the greatest value of the horizontal force that acts on the prism 1 without causing the motion of the system is F = 30.502 (N). The MATLAB representation of the mechanical system is shown in Fig. 5.6.
The MATLAB commands for the graphics are:
Example 5.2
The rod \(A\!B\) of length \(l\) shown in Fig. 5.7 is supported at end \(B\) on a horizontal surface and at the other end (end \(A\)) by a inclined surface which makes an angle \(\alpha \) with the horizontal. The coefficient of static friction between the rod and the inclined surface and the horizontal surface is \(\mu \). The weight of the rod is \(G=m\!g\). The end \(A\) of the rod (supported by the inclined surface) is positioned in such a way that the angle between the rod and the horizontal supporting surface is equal to \(\beta \). The end \(A\) of the rod can slid down on the inclined plane. A force \(F\) which has its directions parallel with the rod is applied at the left end \(A\) of the rod as shown in Fig. 5.7. Determine the greatest value of \(F\) without causing the motion of the rod. For the numerical example use: \(l=1\) m, \(m=10\) kg, \(\mu = 0.2\), \(\beta = \pi /6\) rad, \(\alpha = \pi /4\) rad, and \(g=9.81\) m/s\(^2\).
Solution
The frictional force at the contact point of the end of the rod with the inclined plane is equal to the product of the static coefficient of friction with the normal force between that same end of the rod and the inclined surface. The normal force is always perpendicular at the contact point to the inclined plane, while the friction force is parallel to the inclined plane. As the direction of the frictional force must resist the tendency to slip, the frictional force must be acting “up” the inclined plane. At the other end of the rod resting on a horizontal surface. The force exerted by the horizontal surface must be vertical and the frictional force is equal to the product of the static coefficient of friction with the normal force as shown in Fig. 5.8.
The weight \(\mathbf{G}\) is also a vertical force. The sum of all the forces acting on the left end \(A\) can be expressed as
where \( \mathbf{N}_{A}\) is the of force of the ground (prism) on the rod at \(A\), \( \mathbf{F}_{fA}\) is the friction force between the prism and the rod at \(A\), \({F}_{fA}=\mu \,{N}\!_A\), \(\mathbf{F}\) is the external force along the rod at \(A\), \( \mathbf{N}\!_{B}\) is the of force of the horizontal surface (ground) on the rod at \(B\), \(\mathbf{N}_{B} \perp x-\)axis, \( \mathbf{F}_{fB}\) is the friction force between the ground and the rod at \(B\), \( {F}_{fB}=\mu \,{N}\!_B\), and \(\mathbf{G}_{2}\) is the weight of the rod. The MATLAB commands for the forces on the rod are:
The sum of the moments of all forces about the left end \(A\) of the rod can be expressed as
The scalar equilibrium equations in MATLAB are:
The normal reactions are:
and the greatest value of \(F\) without causing the motion of the rod is
The MATLAB representation of the mechanical system is shown in Fig. 5.9.
5.5 Technical Applications of Friction: Screws
A screw thread is a uniform wedge-shaped section in the form of a helix on the external or internal surface of a cylinder (straight thread) or a cone (taper thread). The basic arrangement of a helical thread wound around a cylinder is illustrated in Fig. 5.10.
The terminology of an external screw threads is:
-
pitch denoted by \(p\) is the distance, parallel to the screw axis, between corresponding points on adjacent thread forms having uniform spacing.
-
major diameter denoted by \(d\) is the largest (outside) diameter of a screw thread.
-
minor diameter denoted by \(d_r\) or \(d_1\), is the smallest diameter of a screw thread.
-
pitch diameter denoted by \(d_m\) or \(d_2\) is the imaginary diameter for which the width of the threads and the grooves are equal.
The lead denoted by \(l\) is the distance the nut moves parallel to the screw axis when the nut is given one turn (distance a threaded section moves axially in one revolution). A screw with two or more threads cut beside each other is called a multiple-threaded screw. The lead is equal to twice the pitch for a double-threaded screw, and up to 3 times the pitch for a triple-threaded screw. The pitch\(p\), lead \(l\), and lead angle \(\lambda \) are represented in Fig. 5.11.
Figure 5.11a shows a single thread right-hand screw and Fig. 5.11b shows a double-threaded left-hand screw. If a thread traverses a path in a clockwise and receding direction when viewed axially, it is a right-hand thread. All threads are assumed to be right-hand, unless otherwise specified.
Metric threads are specified by the letter M preceding the nominal major diameter in millimeters and the pitch in millimeters per thread. For example: M 14 \(\times \) 2, M is the SI thread designation, 14 mm is the outside (major) diameter, and the pitch is 2 mm per thread. Screw size in the Unified system is designated by the size number for major diameter (in.), the number of treads per in., and the thread form and series, like this: \(\displaystyle \frac{5^{\prime \prime }}{8}\,-\,18\), UNF \(\displaystyle \frac{5^{\prime \prime }}{8}\) is the outside (major) diameter where the double tick marks mean inches, and 18 threads per in.
5.5.1 Power Screws
Power screws are used to convert rotary motion to linear motion of the meeting member along the screw axis. These screws are used to lift weights (screw-type jacks) or exert large forces (presses, tensile testing machines). The power screws can also be used to obtain precise positioning of the axial movement.
A square-threaded power screw with a single thread having the pitch diameter \(d_m\), the pitch \(p\), and the helix angle \(\lambda \) is considered in Fig. 5.12. A square thread profile is shown in Fig. 5.13.
Consider that a single thread of the screw is unrolled for exactly one turn. The edge of the thread is the hypotenuse of a right triangle and the height is the lead. The base of the right triangle is the circumference of the pitch diameter circle (Fig. 5.14). The lead angle \(\lambda \) is the helix angle of the thread. The screw is loaded by an axial compressive force \(F\) (Figs. 5.12 and 5.14). The force diagram for lifting the load is shown in Fig. 5.14a, (the force \(P_r\) is positive). The force diagram for lowering the load is shown in Fig. 5.14b, (the force \(P_l\) is negative). The friction force is
where \(\mu \) is the coefficient of dry friction and \(N\) is the normal force. The friction force is acting opposite to the motion. The equilibrium of forces for raising the load gives
Similarly, for lowering the load one may write the equations
Eliminating \(N\) and solving for \(P_r\)
and for lowering the load
Using the relation
and dividing the equations by \(\cos \lambda \) one may obtain
The moment required to overcome the thread friction and to raise the load is
The moment required to lower the load (and to overcome a part of the friction) is
When the lead, \(l\), is large or the friction, \(\mu \), is low the load will lower itself. In this case the screw will spin without any external effort, and the moment \(M_l\) in Eq. (5.12) will be negative or zero. When the moment is positive, \(M_l>0\), the screw is said to be self-locking. The condition for self-locking is
Dividing both sides of this inequality by \(\pi ~d_m\), and using \(l/(\pi \,d_m) = \tan \lambda \), yields
The self-locking is obtained whenever the coefficient of friction is equal to or greater than the tangent of the thread lead angle.
The moment, \(M_0\), required only to raise the load when the friction is zero, \(\mu = 0\), is obtained from Eq. (5.11):
The screw efficiency \(e\) can be defined as
For square threads the normal thread load, \(F\), is parallel to the axis of the screw. The preceding equations can be applied for square threads.
5.5.2 Force Analysis for a Square-Threaded Screw
Consider a square-threaded jack under the action of a axial load \(F\) and a moment \(M\) about the axis of the screw, Fig. 5.15. The screw has the mean radius \(r_m\) and the lead \(l\). The force exerted by the frame thread on the screw thread is \(R\). The angle \(\theta \) made by \(R\) with the normal to the thread is the angle of friction (see Fig. 5.15)
The unwrapped thread of the screw shown in Fig. 5.15 is for lifting the load. The force equilibrium equation in the axial direction is
where \(\lambda \) is the helix angle, \(\tan \lambda = l/(2 ~\pi ~r_m)\). The moment of \(R\) about the vertical axis of the screw is \(R~r_m~\sin (\lambda +\theta )\). The moment equilibrium equation for the screw becomes
Combining the expression for \(F\) and \(M\) gives
The force required to push the thread up is \(P=M/r_m\). The moment required to lower the load by unwinding the screw is obtained in a similar manner:
If \(\theta <\lambda \) the screw will unwind by itself.
In general, when the screw is loaded axially, a thrust bearing or thrust collar may be used between the rotating and stationary links to carry the axial component (Fig. 5.16). The load is concentrated at the mean collar diameter \(d_c\). The moment required is
where \(\mu _c\) is the coefficient of collar friction.
Example 5.3
A square-thread power screw, as shown in Fig. 5.17 has the major diameter \(d = 38\) mm and the pitch \(p = 6\) mm. The coefficient of friction of the thread is \( \mu = 0.08\) and the coefficient of collar friction is \(\mu _c = 0.1\). The mean collar diameter is \(d_c = 45\) mm. The external load on the screw is \(F = 9\) kN. Find: (a) the lead, the pitch (mean) diameter and the minor diameter; (b) the moment required to raise the load; (c) the moment required to lower the load; (d) the efficiency of the device.
Solution
(a) From Fig. 5.13:
the minor diameter is \(d_r=d-p\)
the pitch (mean) diameter is \(d_m=d-p/2\)
the lead is\(l = p,\)
or:
(b) The moment required to raise the load is
and:
(c) The moment required to lower the load is
and:
The sef-locking condition:
The screw is self-locking sf = 2.796.
(d) The overall efficiency is calculated with
and:
5.6 Problems
-
5.1
Find the orientation angle \(\theta \) of the force \(P\) for the smallest possible force \(P\) that can be applied so that the body shown in Fig. 5.18 is on the verge of moving. The body has weight the mass \(m\) and the coefficient of static friction at the surface is \(\mu _s=0.4\).
-
5.2
The car shown in Fig. 5.19 has the mass \(m\), the center of mass at \(C\), and travels along a track with a constant speed. Find the greatest slope \(\theta \) of the track without causing the car to tip or to slip. The coefficient of static friction between the road and the car is \(\mu \). For the numerical example use: \(m= 2000\) kg, \(\mu = 0.3\), \(l=1.75\) m, \(h= 0.5\) m, and \(g=9.81\) m/s\(^2\).
-
5.3
A uniform bar of mass \(m\) and length \(l\) is placed on a rough wall at \(A\) and on a smooth floor at \(B\) at shown in Fig. 5.20. The coefficient of static friction between the bar and the wall is \(\mu \). The distance \(O\!B=d\) is given. Find if the bar will remain in the initial position when it is released. For the numerical example use: \(\mu = 0.4\), \(l=1\) m, \(d= OB= 0.3\) m, and \(g=9.81\) m/s\(^2\).
-
5.4
The block 1, shown in Fig. 5.21, has the mass \(m\) and is placed on a rough wall. Find the minimum force\(F\) required to move the block of mass \(m\). The coefficient of static friction is \(\mu \). The angle of the two wedges 2 and 3 is \(\alpha \). For the numerical example use: \(m=80\) kg, \(\mu = 0.4\), \(\alpha =\pi /180\) rad, and \(g=9.81\) m/s\(^2\).
-
5.5
The wedge 3, shown in Fig. 5.22, has the mass \(2\,m\). The wedges 2 has the mass \(m\). Find the minimum force \(F\) required to move the wedge 3. The coefficient of static friction is \(\mu \). The angle of the wedges is \(\alpha \). For the numerical example use: \(m=10\) kg, \(\mu = 0.2\), \(\alpha =15^\circ \) rad, and \(g=9.81\) m/s\(^2\).
-
5.6
A double square-thread power screw has a pitch (mean) diameter of 30 mm and a pitch of 6 mm. The coefficient of friction of the thread is 0.1 and the coefficient of collar friction is also 0.2. The mean collar diameter is 40 mm. The external load on the screw is 8 kN. Determine the moment required to lower the load and the overall efficiency.
-
5.7
A power screw has a double square thread with a mean diameter of 50 mm and a pitch of 8 mm. The coefficient of friction in the thread is 0.15. Determine if the screw is self-locking.
-
5.8
A triple-thread screw is used in a jack to raise a load of 3000 lb. The major diameter of the screw is 4 in. A plain thrust collar is used. The mean diameter of the collar is 5 in. The coefficient of friction of the thread is 0.08 and the coefficient of collar friction is 0.2. Determine: (a) the screw pitch, lead, thread depth, mean pitch diameter, and helix angle; (b) the starting moment for raising and for lowering the load; (c) the efficiency of the jack.
5.7 Programs
5.7.1 Program 5.1
5.7.2 Program 5.2
5.7.3 Program 5.3
References
P. Appell, Traité de mécanique rationnelle (Gauthier-Villars, Paris, 1955)
M. Atanasiu, Mechanics (EDP, Bucharest, 1973)
H. Baruh, Analytical Dynamics (WCB/McGraw-Hill, Boston, 1999)
G. Baumann, Mathematica for Theoretical Physics: Classical Mechanics and Nonlinear Dynamics (Springer, New York, 2005)
G. Baumann, Mathematica for Theoretical Physics: Electrodynamics, Quantum Mechanics, General Relativity and Fractals (Springer, New York, 2005)
F.P. Beer, E.R. Johnston, Vector Mechanics for Engineers: Statics and Dynamics 5th edn. (McGraw-Hill Publishing Company, New York, 1988)
F.P. Beer, E.R. Johnston, D.F. Mazurek, Vector Mechanics for Engineers: Statics 10th edn. McGraw-Hill Publishing Company, New York, 2012)
A.M. Bedford, W. Fowler, K.M. Liechti, Statics and Mechanics of Materials (Prentice Hall, Inc., Upper Saddle River, NJ, 2002)
A.M. Bedford, W. Fowler, Engineering Mechanics: Statics 5th edn. (Prentice Hall, Inc., Upper Saddle River, NJ, 2007)
A.P. Boresi, R.J. Schmidt, Engineering Mechanics: Statics (PWS Publishing Company, Boston, 2000)
M.I. Buculei, Mechanics (University of Craiova Press, Craiova, 1974)
M.I. Buculei, D. Bagnaru, G. Nanu, D.B. Marghitu, Analysis of Mechanisms with Bars (Scrisul romanesc, Craiova, 1986)
I. Stroe et al., Analytical Mechanics Problems (University Politehnica of Bucharest, Bucharest, 1997)
V. Ceausu, N. Enescu, F. Ceausu, Mechanics Problems (Printech, Bucharest, 1999)
S.J. Chapman, MATLAB Programming for Engineers (Thomson Engineering, 2007).
S. Attaway, MATLAB: A Practical Introduction to Programming and Problem Solving (Butterworth-Heinemann, Elsevier, Amsterdam, 2012)
D.M. Etter, D.C. Kuncicky, Introduction to MATLAB for Engineers and Scientists (Prentice Hall, Inc., Upper Saddle River, NJ, 1996)
C. Iacob, Theoretical Mechanics (EDP, Bucharest, 1980)
J.H. Ginsberg, Advanced Engineering Dynamics (Cambridge University Press, Cambridge, 1995)
D.T. Greenwood, Principles of Dynamics (Prentice-Hall, Inc., Englewood Cliffs, NJ, 1998)
L.E. Goodman, W.H. Warner, Statics (Dover Publications, Inc., New York, 2001)
R.C. Hibbeler, Engineering Mechanics: Statics and Dynamics 13th edn. (Prentice-Hall, Inc., Upper Saddle River, NJ, 2013)
T.R. Kane, Analytical Elements of Mechanics, vol. 1 (Academic Press, New York, 1959)
T.R. Kane, Analytical Elements of Mechanics, vol. 2 (Academic Press, New York, 1961)
T.R. Kane, P.W. Likins, D.A. Levinson, Spacecraft Dynamics (McGraw-Hill, New York, 1983)
T.R. Kane, D.A. Levinson, Dynamics (McGraw-Hill, New York, 1985)
R. Maeder, Programming in Mathematica (Addison-Wesley Publishing Company, Redwood City, CA, 1990)
N.H. Madsen, Statics and dynamics, class notes, available at http://www.eng.auburn.edu/users/nmadsen/
D.B. Marghitu, Mechanical Engineer’s Handbook (Academic Press, San Diego, CA, 2001)
D.B. Marghitu, M.J. Crocker, Analytical Elements of Mechanisms (Cambridge University Press, Cambridge, 2001)
D.B. Marghitu, Kinematic Chains and Machine Component Design (Elsevier, Amsterdam, 2005)
D.B. Marghitu, Mechanisms and Robots Analysis with MATLAB (Springer, New York , 2009)
D.B. Marghitu, M. Dupac, Advanced Dynamics: Analytical and Numerical Calculations with MATLAB (Springer, New York, 2012)
D.B. Marghitu, Statics and dynamics, class notes, available at http://www.eng.auburn.edu/users/marghitu/
D.J. McGill, W.W. King, Engineering Mechanics: Statics and an Introduction to Dynamics (PWS Publishing Company, Boston, 1995)
J.L. Meriam, L.G. Kraige, Engineering Mechanics: Statics 7th edn. (John Wiley & Sons, New York, 2011)
R.L. Mott, Machine Elements in Mechanical Design (Prentice Hall, Upper Saddle River, NJ, 1999)
R.L. Norton, Machine Design (Prentice-Hall, Upper Saddle River, NJ, 1996)
L.A. Pars, A Treatise on Analytical Dynamics (John Wiley & Sons, New York, 1965)
M. Plesha, G. Gray, F. Costanzo, Engineering Mechanics: Statics 2nd edn. (McGraw-Hill, New York, 2012)
M. Radoi, E. Deciu, Mechanics (EDP, Bucharest, 1981)
W.F. Riley, L.D. Sturges, Engineering Mechanics: Statics 2nd edn. (John Wiley & Sons, Inc., New York, 1995)
A. Ruina, R. Pratap, Introduction to Statics and Dynamics (Oxford University Press, Oxford, 2002)
A. Ripianu, P. Popescu, B. Balan, Technical Mechanics (EDP, Bucharest, 1979)
I.H. Shames, Engineering Mechanics Statics 4th edn. (Prentice Hall, Inc., New Jersey, 1996)
S.D. Sheppard, B.H. Tongue, Statics: Analysis and Design of Systems in Equilibrium (John Wiley & Sons, New York, 2005)
D. Smith, Engineering Computation with MATLAB (Pearson Education, Upper Saddle River, NJ, 2008)
R.W. Soutas-Little, D.J. Inman, Engineering Mechanics: Statics and Dynamics (Prentice-Hall, Upper Saddle River, NJ, 1999)
R.W. Soutas-Little, D.J. Inman, D. Balint, Engineering Mechanics: Statics (Cengage Learning, Independence, KY, 2007)
S. Staicu, Theoretical Mechanics (EDP, Bucharest, 1998)
A. Stan, M. Grumazescu, Mechanics Problems (EDP, Bucharest, 1973)
J. Sticklen, M.T. Eskil, An Introduction to Technical Problem Solving with MATLAB (Great Lakes Press, Wildwood, MO, 2006)
A. Stoenescu, G. Silas, Theoretical Mechanics (ET, Bucharest, 1957)
J.H. Jackson, H.G. Wirtz, Schaum’s Outline of Theory and Problems of Statics and Strength of Materials (McGraw-Hill, New York, 1983)
The MathWorks: https://www.mathworks.com/
Statics eBook : https://ecourses.ou.edu/
R. Voinea, D. Voiculescu, V. Ceausu, Mechanics (EDP, Bucharest, 1983)
V. Valcovici, S. Balan, R. Voinea, Theoretical Mechanics (ET, Bucharest, 1959)
K.J. Waldron, G.L. Kinzel, Kinematics, Dynamics, and Design of Machinery (John Wiley & Sons, New York, 1999)
H.B. Wilson, L.H. Turcotte, D. Halpern, Advanced Mathematics and Mechanics Applications Using MATLAB (Chapman & Hall/CRC, Boca Raton, 2003)
J.H. Williams Jr, Fundamentals of Applied Dynamics (John Wiley & Sons, New York, 1996)
S. Wolfram, Mathematica (Wolfram Media/Cambridge University Press, Cambridge, 1999)
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2013 Springer London
About this chapter
Cite this chapter
Marghitu, D.B., Dupac, M., Madsen, N. (2013). Friction. In: Statics with MATLAB®. Springer, London. https://doi.org/10.1007/978-1-4471-5110-4_5
Download citation
DOI: https://doi.org/10.1007/978-1-4471-5110-4_5
Published:
Publisher Name: Springer, London
Print ISBN: 978-1-4471-5109-8
Online ISBN: 978-1-4471-5110-4
eBook Packages: EngineeringEngineering (R0)