Notes on Dynamics | Cal State LA, Exams of Dynamics

These notes are a supplement to FE Reference Handbook, 9.5 Version, for Computer- ... See motion equations in the 9.5 Handbook on pp. 78‐79.

Typology: Exams

2022/2023

Uploaded on 02/28/2023

shekhar_hin
shekhar_hin 🇺🇸

4.9

(9)

226 documents

1 / 23

Toggle sidebar

This page cannot be seen from the preview

Don't miss anything!

bg1
Notes on Dynamics
by
Stephen F. Felszeghy
CSULA Prof. Emeritus of ME
These notes are a supplement to FE Reference Handbook, 9.5 Version, for Computer-
Based Testing, NCEES, June 2018, pp. 77-84.
These notes were prepared for the FE/EIT Exam Review Course class meeting held on
Feb. 8, 2020, 9:00 a.m. to 4:00 p.m.
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13
pf14
pf15
pf16
pf17

Partial preview of the text

Download Notes on Dynamics | Cal State LA and more Exams Dynamics in PDF only on Docsity!

Notes on Dynamics

by

Stephen F. Felszeghy

CSULA Prof. Emeritus of ME

These notes are a supplement to FE Reference Handbook , 9.5 Version, for Computer-

Based Testing, NCEES, June 2018, pp. 77-84.

These notes were prepared for the FE/EIT Exam Review Course class meeting held on

Feb. 8, 2020, 9:00 a.m. to 4:00 p.m.

Dynamics

Kinematics – deals with motion alone apart from considerations of

force and mass.

Kinetics – relates unbalanced forces with changes in motion.

Kinematics of Particles

Rectilinear Motion of a Particle

Suppose

v = v x

; apply “Chain Rule”:

dv

dt

= a =

dv

dx

dx

dt

a =

dv

dx

v

Determination of Motion of a Particle

Integrate differential relations:

Motion

Kinematics

Kinetics

Unbalanced Forces

Position coordinate

(Rectilinear displacement):

x = f ( t ) → x = x ( t )

Velocity:

v =

dx

dt

x

Acceleration:

a =

dv

dt

d

2

x

dt

2

= ˙ x ˙

dx = v dt

dv = a dt

v dv = a dx

O P

  • x

x

Rectangular Components

Application: See projectile motion in the 9.5 Handbook on p. 79.

Motion Relative to Translating Reference Axes

v (tangent to path)

patpath)

a

r

P

y

x

O

Path

Position vector:

r = r ( t )

(Vector function)

Velocity:

v =

d r

dt

r

Acceleration:

a =

d v

dt

d

2

r

dt

2

= ˙ r ˙

y

z

x

j

k

i

O

Position vector:

r = x i + y j + z k

Velocity:

v = x ˙ i + y ˙ j + ˙ z k

Acceleration:

a = ˙ x ˙ i + ˙ y ˙ j + ˙ z ˙ k

We write:

v

x

x , etc.

a

x

x , etc.

y

O

B

A

r

A

r

A / B

x

y’

x’

r

B

“Translating” means x’ – y’ axes

move but remain parallel to

x – y axes.

r

A

= r

B

  • r

A / B

r

A

r

B

r

A / B

v

A

= v

B

  • v

A / B

a

A

= a

B

  • a

A / B

Tangential and Normal Components

v =

d r

dt

ds

dt

e

t

= v e

t

a =

d v

dt

d

2

r

dt

2

d

2

s

dt

2

e

t

v

2

ρ

e

n

dv

dt

e

t

v

2

ρ

e

n

= a

t

e

t

+ a

n

e

n

= a

t

+ a

n

Radial and Transverse Components

a =

v =

r =

rr

θ

2

( )

e

r

  • r

θ + 2

r

θ

( )

e

θ

v

r

r

v

θ

= r

θ

a

r

= ˙ r ˙ − r

θ

2

a

θ

= r

θ + 2 r ˙

θ

e

n

r

P

y

x

O

Path

s

e

t

C

Center of

curvature

CP = ρ = radius of curvature

e

t

= unit vector tangent to path

e

n

= unit vector normal to path

pointing to C

s = directed distance along path

Polar coordinates of P :

r , θ

e

r

= unit vector in r direction

e

θ

= unit vector perpendicular to r

in direction of increasing θ

r = r e

r

v =

r =

r e

r

  • r

θ e

θ

y

O

x

e

θ

e

r

θ

Path

r = r e

r

P

In either system, W = mg , where

W = weight

g = acceleration due to gravity

At surface of earth: (SI) g = 9.807 m/s

2

(USCS) g = 32.174 ft/s

2

AVOID: lbf, lbm

Equations of Motion: Rectangular Components

F

x

= m a

x

F

y

= m a

y

Equations of Motion: Tangential and Normal Components

y

y

O

O

x

x

F

y

F

x

P

P

m a

y

m a

x

FBD

KD

F

t

= m a

t

F

n

= m a

n

FBD

KD

y y

x

x

O

O

F

n

F

t

P

P

m a

n

m a

t

Path

Equations of Motion: Radial and Transverse Components

Kinetics of Particles: Energy Methods

Above result is the principle of work and energy. Units: (SI) N⋅m = J; (USCS) ft⋅lb

y

O

O

x x

r

r

θ

θ

Path

y

F

θ

F

r

P

P

m a

θ

m a

r

F

r

= m a

r

F

θ

= m a

θ

FBD

KD

y

x

Position 2

Position 1

r

2

r

r

1

O

P

F

s

Path

The work done by F on the particle

during a finite movement of the

particle along a curved path from

position 1 to position 2 is

U

1 → 2

U

1 → 2

= Fd r

r

1

r

2

(Line integral)

It can be shown:

U

1 → 2

= F

t

s

1

s

2

ds

mv

2

2

mv

1

2

Let T =

mv

2

= kinetic energy of particle

Then,

U

1 → 2

= T

2

− T

1

= Δ T

or T

2

= T

1

+ U

1 → 2

Position 2

Position 1

v

2

v

1

F

t

F

n

y

x

O

P

s

Summary

The work‐energy equation can now be written as:

U

1 → 2

= Δ T + Δ V

g

+ Δ V

e

where

U

1 → 2

is the work done on the particle by forces other than

gravitational and spring forces.

If

U

1 → 2

above is zero, then:

T

2

+ V

g

( )

2

+ V

e

( )

2

= T

1

+ V

g

( )

1

+ V

e

( )

1

This is the law of conservation of total mechanical energy.

Power and Efficiency

Power is the time rate of doing work by a force on a particle.

Power = Fv Units:

SI

N ⋅ m s = J s = W; USCS

hp = 550

ft ⋅ lb

s

η =

power output

power input

= mechanical efficiency

Kinetics of Particles: Momentum Methods

Define angular momentum

H

O

of particle about O :

H

O

= r × m v

y

x

v

t

1

t

2

O

F

P

Path

r

Recall Newton’s 2

nd

law:

F = m a =

d

dt

m v

where

F = resultant force

m v = linear momentum of particle

Then,

H

O

= r × m a = r × F = M

O

or

M

O

H

O

where M

O

= sum of the moments about O of

all forces acting on particle

Equations of Impulse and Momentum

What is the cumulative effect of integrating

F and

M

O

with respect to time

over an interval from

t

1

to

t

2

F dt

t

1

t 2

= d m v

= m v

2

m v

1

m v 2

m v

1

or

m v

1

  • F dt

t

1

t

2

= m v

2

Graphical interpretation:

or

mv

x

1

+ F

x

t 1

t

2

dt = mv

x

2

mv

y

( )

1

+ F

y

t 1

t

2

dt = mv

y

( )

2

Units:

SI

kg ⋅

m

s

= N ⋅ s; USCS

lb ⋅ s

Recall

M

O

d H

O

dt

M

O

t

1

t 2

dt = d H

O

= H

O

2 H

O

( )

1

H O

( )

2

− H

O

1

y

x

O

m v

1

F dt

t 1

t

2

m v

2

Initial

linear

momentum

Linear

impulse

Final

linear

momentum

Note: Angular impulses from internal forces of action and reaction cancel.

If no external forces act from time

t

1

to

t

2

, then

H

O

( )

1

= H

O

( )

2

∑ ∑

and the total angular momentum of the particles is conserved.

Graphical interpretation:

Direct Central Impact

Before

Impact

After

Total linear momentum is conserved during impact:

m

1

v

1

  • m

2

v

2

= m

1

v

1

  • m

2

v

2

O O O

x x

x

y

y y

m

1

v

1

1

m

2

v

2

1

m

3

v

3

1

m

1

v

1

2

m

2

v

2

2

m

3

v

3

2

F dt

t 1

t

2

M

O

dt

t

1

t 2

∑ ∫

m

1

m

1

m

1

m

2

m

2

m

2

v

1

v

2

v

1

v

2

v

1

v

2

v

1

v

2

v

1

v

2

u

Coefficient of restitution : e =

velocity of separation

velocity of approach

v

2

v

1

v

1

v

2

If total kinetic energy is conserved, impact is said to be perfectly elastic and

e = 1 .

If particles stick together after impact,

v

1

v

2

, impact is said to be perfectly

plastic , and

e = 0.

For all other impact cases,

0 ≤ e ≤ 1.

A special case occurs when

m

1

= m

2

, collision is elastic ,

v

1

0 , and

v

2

Then,

v

1

= 0 and

v

2

= v

1

Kinematics of Rigid Bodies

Types of plane motion:

Rectilinear translation

Curvilinear translation

Fixed‐axis rotation

A

1

B

1

A

2

B

2

A

1

B

1

A

2

B

2

A

1

A

2

θ

Note: In r θ coordinates,

v

r

v

θ

= ω r

a

r

= − ω

2

r

a

θ

= α r

In t n axes,

v = ω r

a

n

= ω

2

r

a

t

= α r

General Plane Motion – Absolute and Relative Velocity and Acceleration

Graphical interpretation:

Plane Motion Translation with

v

B

Rotation about B

with ω

Plane Motion Translation with

a

B

Rotation about B

with ω and α

Axes x – y translate with their

origin attached to particle B.

r A

= r B

  • r rel

v

A

= v

B

  • ω × r

rel

a A

= a B

  • α × r rel

  • ω × (ω × r rel

= a B

  • α × r rel

− ω

2

r rel

Y

X

r

A

O

y

x

B

A

r

B

r

rel

α

ω

ω × r

rel

ω × r

rel

v

A

v

A

v

B

v

B

v

B

v

B

A

A A

B

B

B

a

A

a

B

a

B

a

B

a

A

a

B

α × r

rel

α × r rel

− ω

2

r

rel

B

B B

A

A

A

Instantaneous Center of Rotation in Plane Motion

Suppose

v

B

in the previous analysis. Then,

v A

= ω × r rel

This result implies the body is rotating for an instant about point B. Such a

point is called an instantaneous center of rotation (I.C.R.). Such a point can be

determined, as follows, if the velocities of two different particles in a body

are known.

Note: The location of the I.C.R. changes with time in general. Hence,

a

ICR

in general!

Plane Motion of a Particle Relative to a Rotating Frame

Y

X

O

x

y

B

A

r

A

r

€ B

r

rel

ω

α

Axes x – y are body‐fixed

axes, which have angular

velocity ω and angular

acceleration α.

Particle A moves relative to

the body‐fixed axes x – y.

The relative position vector

of A referenced to the x – y

axes is

r

rel

= x i + y j

A

v

A

v

B

B

I.C.R

v

A

v

B

A

B

I.C.R

v

A

A

v

B

B

I.C.R

where: m = total mass

c = center of mass

I

c

= mass moment of inertia about axis

through c parallel to z axis

p = any moment center in x – y plane

In component form:

F

x

= ma

cx

F

y

= ma

cy

M

c

= I

c

Noncentroidal Rotation

FBD KD

M

q

= I

c

α + ρ

qc

× m a

ct

= I

q

α

where

I

q

= mass moment of inertia about axis through q

parallel to z axis.

Laws of Friction

N

F

P

W

g

Block is initially at rest when force P is

applied and its magnitude is progressively

increased from zero. As long as

P = F < μ

s

N

the block will not slide.

μ

s

= coefficient of static friction.

c c

F

1

Q

F

2

I

c

α

ρ qc

(bearing

force)

Center

of

rotation

y

x

O

y

x

O

q q

m a

ct

m a

cn

When

P = F = μ

s

N , the block starts to slide, and F becomes:

F = μ

k

N

where

μ

k

= coefficient of kinetic friction ,

μ

k

< μ

s

Kinetics of Rigid Bodies: Energy Methods

For a body in plane motion, the work done on the body by all external forces

F

i

is

U

1 → 2

= F

i

r

i

( )

1

r

i

( )

2

∑ ∫

d r

i

when the body is displaced from position 1 to position 2.

For a body in plane motion, the kinetic energy is

T =

mv

c

2

I

c

ω

2

For a body in plane motion, the work done on the body by a couple M is

U

1 → 2

= M d θ

θ

1

θ

2

when the body is displaced from position 1 to position 2.

In general,

U

1 → 2

m v

c

2

2

I

c

ω

2

2

m v

c

1

2

I

c

ω

1

2

= T

2

− T

1

= Δ T

or

T

2

= T

1

+ U

1 → 2

If a gravitational force W acts on the body, and/or a linearly‐elastic spring

force, then the work‐energy equation can be written as:

U

1 → 2

= Δ T + Δ V

g

+ Δ V

e

where

U

1 → 2

now excludes gravitational and spring forces. If

U

1 → 2

above is

zero, total mechanical energy is conserved.