EMEM:359  Dynamics Session:19983


Instructor: Dr. P.Venkataraman             Tel:     X6975
Room:     17-3619                                 Email: pnveme@rit.edu

URL: http://people.rit.edu/pnveme/EMEM359.html( for the course)

http://people.rit.edu/pnveme/Dr. Venkat's homepage

Office Hrs: MWF 10 - 10.45, 2 - 2.45
Text:       Engineering Mechanics: Dynamics, R.C.Hibbler

Prerequisites: EMEM 336 Statics
        Topics: Differential and Integral Calculus
                        Differential Equations
                        Vector Algebra

Course Objective: The course will help understand problems in Dynamics
Grading:     First Test:           20 %
                      Second Test:     25 %
                       Final:           35 %
                       HW:            20 %

Home Work: Home Work assigned for the week (MWF) is due following Wednesday

Based on the first homework set the requirement/grading  for homework is ammended as follows (3/23/99)

1.  No figure  : 0 marks
2.  Work unclear and not in order:  not graded
3.  No straight edge : -30%
4.  No unit vectors  :  -20 %
5.  No FBD/AD :  0 marks
6.  No units on the final result :  -10%

Formulae/Relations

 
Lecture
HW Due on
Class Work
Home Work
3/8/99 3/17/99 Sec 12.1 - 12.3 Prob. 12/2, 12/16, 12/44, 12/64 12/9, 12/27, 12/43, 12/55
Read Ch. 12
3/10/89 3/17/99 Sec. 12.4 - 12.7, 
Prob. 12/70, 12/78, 12/91
12/73, 12/80, 12/92, 12/117
Read Ch. 12
3/12/99 3/17/99 Prob. 12/107, 12/112 12/121,  12/127
Read Ch. 12
3/15/99 3/24/99 Sec. 12.8,  Prob. 12/152, 12/160
Spherical Coord.   Sp. prob
12/139, 12/151, 12/155, 12/170
Read Ch. 12
 3/17/99 3/24/99  Sec. 12.9, 12.10.  Prob.  12/174,12/184.12/200, 12/206   12/175, 12/183, 12/201, 12/205, Read Ch. 13
 3/19/99 3/24/99 Sec. 13.1 - 13.4,   Prob. 13/4, 13/22   13/5, 13/15  Read Ch. 13
 3/22/99 3/31/99  Sec. 13.5 - 13.6,  Prob. 13/38, 13/58, 13/76, 13/91   13/41, 13/53, 13/63, 13/69
 3/24/99 3 /31/99  Sec. 13-7 (curiosity) 13/101, 13/110, 12/127

Test # 1: Ch. 12 , 13  - 1 Formula sheet, closed book
Friday, April 2, 1999

13/79, 13/86, 13/102, 13/108        Read Ch. 14
3/26/99 3/31/99 Sec. 14.1 14.2   Prob. 14.3 14/5,  14/9   Read Ch. 14
3/29/99 4/7/99 Sec. 14.4  Prob.  14/3, 14/15, 14/29, 14/51 14/13, 14/25, 14/30, 14/39     Read Ch. 14
3/31/99 4/7/99 Sec. 14.5, 14.6     Prob. 14/63,  14/77, 14/81 14/45, 14/58, 14/75, 14/79          Read Ch. 15
4/2/99 TEST # 1
4/5/99 4/14/99 Sec. 15.1 - 15.3   Prob. 14/90, 15/4, 15/18, 15/26 15/6, 15/17, 15/21, 15/29    Read Ch. 15
4/7/99 4/14/99 Sec 15.4   Prob. 15/36,  15/48  15/34, 15/51, 15/57, 15/58     Read Ch. 15
4/9/99 4/14/99 Prob, 15/61, 15/66 15/74, 15/79      Read Ch. 15
4/12/99 4/21/99 Sec. 15.5 - 15.7  Prob. 15/66, 15/91, 15/106 15/83, 15/93, 15/102, 15/103  Read Ch. 16
4/14/99 4/21/99 Sec 16.1 - 16.3     Prob. 16/4,  16/7  16/3, 16/6. 16/9, 16/22   Read Ch. 16
4/16/99 4/21/99 Sec 16.5  Prob 16/58 16/51, 16/59  Read Ch. 16
4/19/99 4/28/99 Sec. 16.6 - 16.7   Prob. 16/62,  16/90, 16/95
Test # 2 Closed Book/Formula Sheet
          Chapters 14/15
          4/30/99 - Friday
16/63, 16/70, 16/88, 16/93  Reda Ch. 16
4/21/99 Review Class - 
4/23/99 4/28/99 Review Section 16.7   Prob. 16/109, 16/112 16/107, 16/121 or 16/127
4/26/99 5/5/99 Sec 17. - 17.3,  Prob. 16/112, 16/124, 17/12, 17/21 16128, 16/129, 17/1, 17/7
4/28/99 5/5/99 Prob. 17/27, 17/35. 17/50  17/26, 17/32, 17/39, 17/45  Read Ch. 17
4/30/99 Test # 2
5/3/99 5/12/99 Sec 17.4.  17/62, 17/77, 17/84  17/58,  17/61, 17/81  Read Ch. 17
5/5/99 5/12/99 Lecture of simple Plane rigid body - pendulum/inverted pendulum.  Discussion of damping stability/instability and need for control. Invited demonstration of a working inverted pendulum Graphical solution of your own stick pendulum design using proper values for material properties and geometry
5/7/99 5/12/99 Sec 17.5 , Prob. 17/92, 17/115 Prob. 17/93, 17/115  Read Ch. 18
5/10/99 Sec. 18.1 - 18.4, Prob.  18/10, 18/23, 18/28 Prob. 18/2, 18/14, 18/21, 18/30  Read Ch. 18
5/12/99 Sec. 18.5  Prob. 18/39, 18/44, 18/50 Prob. 18/35, 18/37, 18/61
Final       5/18/99      2.15 - 4.15      09-2119

 
 

Relations/Formulae

Rectangular Coordinate System [ Click Button to Open in new window - uses Javascript ] 
Normal Tangent Coordinate System [ Click Button to Open in new window - uses Javascript ] 
Cylindrical Coordinate System [ Click Button to Open in new window - uses Javascript ] 
Spherical Coordinate System [ Click Button to Open in new window - uses Javascript ] 
Connected System of Partices [ Click Button to Open in new window - uses Javascript ] 
Relative Motion[ Click Button to Open in new window - uses Javascript ] 
Oblique Impact[ Click Button to Open in new window - uses Javascript ] 
Angular Momentum [ Click Button to Open in new window - uses Javascript ] 
Rigid Body Kinematics [ Click Button to Open in new window - uses Javascript ] 
Rigid Body Kinematics- General Plane Motion [ Click Button to Open in new window - uses Javascript ] 
Rigid Body Kinematics- Acceleration [ Click Button to Open in new window - uses Javascript ] 
Rigid Body - Plane Kinetics[ Click Button to Open in new window - uses Javascript ] 
Rigid Body - Work/Energy[ Click Button to Open in new window - uses Javascript ] 
 
3/8/99 General relations: independent of coordinate system
Position vector:       r(t) [ 2D];    R(t) [3D] 
Velocity vector       v(t) = dR(t)/dt; 
Acceleration vector   a(t) = dv(t)/dt = d2R(t)/dt2

Rectlilinear motion:  [also 1 D motion] - vector representation is an overkill as only one direction is involved
position:             r(t)
vector:                v(t): = dr/dt                       r2-r1 = integral{v(t)dt} between t1,t2
acceleration:     a(t) = dv/dt = d2r/dt         v2-v1 = integral{a(t)dt} between t1,t2

also               a(r)dr = vdv      0.5( v22 -v12  )= integral{a(r)dr} between r1,r2

For convenience - dependence on t is not explicitly transcribed

3/10/99 General Curvilinear Motion:

Position vector:       r(t) [ 2D];    R(t) [3D] 
Velocity vector       v(t) = dR(t)/dt; 
Acceleration vector   a(t) = dv(t)/dt = d2R(t)/dt2

Cartesian/Rectangular Coordinate System:
Coordinates : x, y, z
Unit vectors :   i, j, k

R = x i  + y j  + z k; 
v  = vx i  +  vy j  + vz  k   =      dx/dt i  +  dy/dt j  +  dz/dt k 
a  = ax i  +  ay j  + az  k   =      dv/dt i  +  dvy /dt j  +  dvz  /dt k 
                                       =     d(dx/dt ) /dt i  +  d(dy/dt) /dt j  +  d(dz/dt ) /dt k 

The cartesian coordinate system can be regarded as a vector sum of 
three rectilinear motions in x, y, z, diections

Normal - Tangent - Binormal system
Coordinates:s
Unitvectors: et , en , e b

Normal Tangent Coordinate System [ Click Button to Open in new window - uses Javascript ] 

 

3/15/99 Cylindrical Coordinate System [ Click Button to Open in new window - uses Javascript ] 

Spherical Coordinate System [ Click Button to Open in new window - uses Javascript ] 
 

 3/17/99 Connected System of Partices [ Click Button to Open in new window - uses Javascript ] 

Relative Motion[ Click Button to Open in new window - uses Javascript ] 
 

 3/19/99  Kinetics  ( Force and Motion) [ need a FREE BODY DIAGRAM (FBD) and an ACCELERATION DIAGRAM (AD) for Analysis

Newton's Law : F = m a {independent of coordinate system}

Newton's Law of Gravitation: 

                               F = m1m2 / R2   (The forces are directed along their centers)

Rectangular System: 
 

 3/22/99  Newtons Law:  Normal-Tangent System/Cylindrical System
 3/24/99 Space Motion  - For Information only
 3/26/99  Work and Energy 
3/29/99 Power: P = F . v (Power like Work and Energy is a scalar - It is the scalar or dot product of the two vectors Force and velocity)
Efficiency: = e = ( Powerused/ Poweravailable ):It is always less than one
3/31/99 Conservation of Energy:

     Conservative Forces:  Forces whose work is INDEPENDENT of path but depends on position;
           Examples ; Weight and Elastic Spring force

     Each conservative force can be associated with a potential function (V) which depends on position 
           F  = - grad{ V }

     Vg= potential function due to weight  =  mgy ; m = mass of particle,  g = gravitational acceleration
                                                                              y = distance above datum  (reference for zero potential)
     Work done when the particle moves from A to B  = VgB - VgA

      Ve = potential function/energy due to elastic spring  = 0.5 k x2 ; k = spring constant, x = change from unstretched length
     Work done when the partices moves from A to B and spring is involved = VeB - VeA

 

4/5/99 Impulse and Momentum: This is another integrated form of Newtons Law

4/7/99 Impact occurs when two bodies collide for a short period of time. Information on the value of e , the coefficient of restitution, is necessary to solve impact problems.  While in most problems the conservation of momentum applies to a system of particles, the distribution of momentum is controlled by the coeffiecient of restitution
4/9/99 Oblique Impact [ Click Button to Open in new window - uses Javascript ] 
4/12/99 Angular Impulse and Momentum: [ Click Button to Open in new window - uses Javascript ] 
4/14/99 Rigid Body Kinematics [ Click Button to Open in new window - uses Javascript ] 
4/16/99 Rigid Body Kinematics - General Plane Motion[ Click Button to Open in new window - uses Javascript ] 
4/19/99 Rigid Body Kinematics- Acceleration [ Click Button to Open in new window - uses Javascript ] 
4/26/99 Rigid Body -Plane Kinetics -  [ Click Button to Open in new window - uses Javascript ] 

Plane Translation -  angular acceleration= 0

Plane Rotation - linear acceleration = 0
 

5/10/99 Rigid Body - Work and Energy [ Click Button to Open in new window - uses Javascript ] 
5/13/99 Rigid Body - Work and Energy -Conservation of Energy
U12 (Work by all Non conservative Forces) =  Change in Kinetic Energy   +
                                                                                      Change in Potential Energy