DYNAMICS VECTOR MECHANICS FOR ENGINEERS: DYNAMICS Tenth Edition CHAPTER © 2013 The McGraw-Hill...

48
VECTOR MECHANICS FOR ENGINEERS: DYNAMICS DYNAMICS Tenth Tenth Edition Edition CHAPTER © 2013 The McGraw-Hill Companies, Inc. All rights reserved. 1 8 Ferdinand P. Beer Ferdinand P. Beer E. Russell Johnston, Jr. E. Russell Johnston, Jr. Phillip J. Cornwell Phillip J. Cornwell Lecture Notes: Lecture Notes: Brian P. Self Brian P. Self California Polytechnic State University California Polytechnic State University Kinetics of Rigid Bodies in Three Dimensions

Transcript of DYNAMICS VECTOR MECHANICS FOR ENGINEERS: DYNAMICS Tenth Edition CHAPTER © 2013 The McGraw-Hill...

Page 1: DYNAMICS VECTOR MECHANICS FOR ENGINEERS: DYNAMICS Tenth Edition CHAPTER © 2013 The McGraw-Hill Companies, Inc. All rights reserved. 18 Ferdinand P. Beer.

VECTOR MECHANICS FOR ENGINEERS: DYNAMICSDYNAMICS

Tenth EditionTenth Edition

CHAPTER

© 2013 The McGraw-Hill Companies, Inc. All rights reserved.

18 Ferdinand P. BeerFerdinand P. Beer

E. Russell Johnston, Jr.E. Russell Johnston, Jr.

Phillip J. CornwellPhillip J. Cornwell

Lecture Notes:Lecture Notes:

Brian P. SelfBrian P. SelfCalifornia Polytechnic State UniversityCalifornia Polytechnic State University

Kinetics of Rigid Bodies in Three Dimensions

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Contents

18 - 2

Introduction

Rigid Body Angular Momentum in Three Dimensions

Principle of Impulse and Momentum

Kinetic Energy

Sample Problem 18.1

Sample Problem 18.2

Motion of a Rigid Body in Three Dimensions

Euler’s Equations of Motion and D’Alembert’s Principle

Motion About a Fixed Point or a Fixed Axis

Sample Problem 18.3

Motion of a Gyroscope. Eulerian Angles

Steady Precession of a Gyroscope

Motion of an Axisymmetrical Body Under No Force

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2 - 3

Three dimensional analyses are needed to determine the forces and moments on the gimbals of gyroscopes, the rotors of amusement park rides, and the housings of wind turbines.

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Introduction

18 - 4

GG HM

amF

• The fundamental relations developed for the plane motion of rigid bodies may also be applied to the general motion of three dimensional bodies.

IHG • The relation which was used to determine the angular momentum of a rigid slab is not valid for general three dimensional bodies and motion.

• The current chapter is concerned with evaluation of the angular momentum and its rate of change for three dimensional motion and application to effective forces, the impulse-momentum and the work-energy principles.

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Rigid Body Angular Momentum in Three Dimensions

18 - 5

• Angular momentum of a body about its mass center,

n

iiii

n

iiiiG mrrmvrH

11Δ

• The x component of the angular momentum,

n

iiiiz

n

iiiiy

n

iiiix

n

iiixiziiyixi

n

iiyiiziix

mxzmyxmzy

mzxzxyy

mrzryH

111

22

1

1

ΔΔΔ

Δ

Δ

dmzxdmxydmzyH zyxx 22

zxzyxyxx III

zzyzyxzxz

zyzyyxyxy

IIIH

IIIH

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Rigid Body Angular Momentum in Three Dimensions

18 - 6

zzyzyxzxz

zyzyyxyxy

zxzyxyxxx

IIIH

IIIH

IIIH

• Transformation of into is characterized by the inertia tensor for the body,

GH

zzyzx

yzyyx

xzxyx

III

III

III

• With respect to the principal axes of inertia,

z

y

x

I

I

I

00

00

00

zzzyyyxxx IHIHIH

• The angular momentum of a rigid body and its angular velocity have the same direction if, and only if, is directed along a principal axis of inertia.

GH

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Rigid Body Angular Momentum in Three Dimensions

18 - 7

• The momenta of the particles of a rigid body can be reduced to:

vm

L

momentumlinear

GHG about momentumangular

zzyzyxzxz

zyzyyxyxy

zxzyxyxxx

IIIH

IIIH

IIIH

• The angular momentum about any other given point O is

GO HvmrH

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Rigid Body Angular Momentum in Three Dimensions

18 - 8

• The angular momentum of a body constrained to rotate about a fixed point may be calculated from

GO HvmrH

zzyzyxzxz

zyzyyxyxy

zxzyxyxxx

IIIH

IIIH

IIIH

• Or, the angular momentum may be computed directly from the moments and products of inertia with respect to the Oxyz frame.

n

iiii

n

iiiO

mrr

mvrH

1

1

Δ

Δ

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Principle of Impulse and Momentum

18 - 9

• The principle of impulse and momentum can be applied directly to the three-dimensional motion of a rigid body,

Syst Momenta1 + Syst Ext Imp1-2 = Syst Momenta2

• The free-body diagram equation is used to develop component and moment equations.

• For bodies rotating about a fixed point, eliminate the impulse of the reactions at O by writing equation for moments of momenta and impulses about O.

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Concept Question

2 - 10

At the instant shown, the disk shown rotates with an angular velocity 2 with respect to arm ABC, which rotates around the y axis as shown (1). Determine the directions of the angular momentum of the disc about point A (choose all that are correct).

+x +y +z

-x -y -z

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Concept Question

2 - 11

A homogeneous disk of mass m and radius r is mounted on the vertical shaft AB as shown Determine the directions of the angular momentum of the disc about the mass center G (choose all that are correct).

+x +y +z

-x -y -z

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Kinetic Energy

18 - 12

• Kinetic energy of particles forming rigid body,

)22

2(

Δ

Δ

222212

21

1

2212

21

1

2212

21

xzzxzyyz

yxxyzzyyxx

n

iii

n

iii

II

IIIIvm

mrvm

vmvmT

• If the axes correspond instantaneously with the principle axes,

)( 222212

21

zzyyxx IIIvmT

• With these results, the principles of work and energy and conservation of energy may be applied to the three-dimensional motion of a rigid body.

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Kinetic Energy

18 - 13

• Kinetic energy of a rigid body with a fixed point,

)22

2( 22221

xzzxzyyz

yxxyzzyyxx

II

IIIIT

• If the axes Oxyz correspond instantaneously with the principle axes Ox’y’z’,

)( 22221

zzyyxx IIIT

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Concept Question

2 - 14

22

1

2 zI

At the instant shown, the disk shown rotates with an angular velocity 2 with respect to arm ABC, which rotates around the y axis as shown (1). What terms will contribute to the kinetic energy of the disk (choose all that are correct)?

21

1

2 yI 21

1

2 xI

2 21

1

2mL

21

1

2 zI

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Sample Problem 18.1

18 - 15

Rectangular plate of mass m that is suspended from two wires is hit at D in a direction perpendicular to the plate.

Immediately after the impact, determine a) the velocity of the mass center G, and b) the angular velocity of the plate.

SOLUTION:

• Apply the principle of impulse and momentum. Since the initial momenta is zero, the system of impulses must be equivalent to the final system of momenta.

• Assume that the supporting cables remain taut such that the vertical velocity and the rotation about an axis normal to the plate is zero.

• Principle of impulse and momentum yields to two equations for linear momentum and two equations for angular momentum.

• Solve for the two horizontal components of the linear and angular velocity vectors.

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Sample Problem 18.1

18 - 16

SOLUTION:• Apply the principle of impulse and momentum. Since the initial momenta is zero,

the system of impulses must be equivalent to the final system of momenta.

• Assume that the supporting cables remain taut such that the vertical velocity and the rotation about an axis normal to the plate is zero.

kvivv zx

ji yx

Since the x, y, and z axes are principal axes of inertia,

jmaimbjIiIH yxyyxxG

21212

121

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Sample Problem 18.1

18 - 17

• Principle of impulse and momentum yields two equations for linear momentum and two equations for angular momentum.

• Solve for the two horizontal components of the linear and angular velocity vectors.

xmv0

0xvzvmtF Δ

mtFvz Δ

kmtFv

Δ

x

x

mb

HtbF

2121

21 Δ

mbtFx Δ6

y

y

ma

HtaF

2121

21 Δ

matFy Δ6

jbiamab

tF Δ6

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Sample Problem 18.1

18 - 18

kmtFv

Δ

jbiamab

tF Δ6

jmaimbH yxG

21212

121

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Sample Problem 18.2

18 - 19

A homogeneous disk of mass m is mounted on an axle OG of negligible mass. The disk rotates counter-clockwise at the rate 1 about OG.

Determine: a) the angular velocity of the disk, b) its angular momentum about O, c) its kinetic energy, and d) the vector and couple at G equivalent to the momenta of the particles of the disk.

SOLUTION:

• The disk rotates about the vertical axis through O as well as about OG. Combine the rotation components for the angular velocity of the disk.

• Compute the angular momentum of the disk using principle axes of inertia and noting that O is a fixed point.

• The kinetic energy is computed from the angular velocity and moments of inertia.

• The vector and couple at G are also computed from the angular velocity and moments of inertia.

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Sample Problem 18.2

18 - 20

SOLUTION:

• The disk rotates about the vertical axis through O as well as about OG. Combine the rotation components for the angular velocity of the disk.

ji

21

Noting that the velocity at C is zero,

Lr

krL

jriLji

rv CC

12

12

210

0

jLri

11

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Sample Problem 18.2

18 - 21

• Compute the angular momentum of the disk using principle axes of inertia and noting that O is a fixed point.

jLri

11

kIjIiIH zzyyxxO

002412

12

412

12

21

mrmLIH

LrmrmLIH

mrIH

zzz

yyy

xxx

jLrrLmimrHO

12

412

12

21

• The kinetic energy is computed from the angular velocity and moments of inertia.

2

12

4122

12

21

22221

LrrLmmr

IIIT zzyyxx

212

22

81 6

L

rmrT

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Sample Problem 18.2

18 - 22

jLri

11

• The vector and couple at G are also computed from the angular velocity and moments of inertia.

kmrvm

1

jLrmrimr

kIjIiIH zzyyxxG

241

12

21

j

L

rimrHG

212

21

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Motion of a Rigid Body in Three Dimensions

18 - 23

GHM

amF

• Angular momentum and its rate of change are taken with respect to centroidal axes GX’Y’Z’ of fixed orientation.

• Convenient to use body fixed axes Gxyz where moments and products of inertia are not time dependent.

• Transformation of into is independent of the system of coordinate axes.

GH

• Define rate of change of change of with respect to the rotating frame,

GH

kHjHiHH zyxGxyzG

Then,

GGxyzGG HHH

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Euler’s Eqs of Motion & D’Alembert’s Principle

18 - 24

GGxyzGG HHM

• With and Gxyz chosen to correspond to the principal axes of inertia,

yxyxzzz

xzxzyyy

zyzyxxx

IIIM

IIIM

IIIM

Euler’s Equations:

• System of external forces and effective forces are equivalent for general three dimensional motion.

• System of external forces are equivalent to the vector and couple, . and GHam

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Group Problem Solving

18 - 25

Two L-shaped arms, each weighing 4 lb, are welded at the third points of the 2-ft shaft AB. Knowing that shaft AB rotates at the constant rate = 240 rpm, determine (a) the angular momentum of the body about B, and b) its kinetic energy.

SOLUTION:

• The part rotates about the axis AB. Determine the mass moment of inertia matrix for the part.

• Compute the angular momentum of the disk using the moments inertia.

• Compute the kinetic energy from the angular velocity and moments of inertia.

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Group Problem Solving

2 - 26

244 lb, 0.12422 lb s /ft ,

32.28 in. 0.66667 ft

W m

a

(2 )(240)8 rad/s, 0, 0

60z x y

Given:

Find: HB, T

There is only rotation about the z-axis, what relationship(s) can you use?

( )B x xzH I ( )B y yzH I ( )B z zH I

Split the part into four different segments, then determine Ixz, Iyz, and Iz. What is the mass of each segment?

•Mass of each of the four segments 20.06211 lb s /ft2

mm

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Group Problem Solving

2 - 27

Fill in the table below to help you determine Ixz and Iyz. 1

2

3 4

Ixz Iyz

1

2

3

4

( )( )m a a

( 0.5 )( )m a a

( )(2 )m a a

a=

(0.5 )(2 )m a a

(0.5 )( )m a a

(0)( )m a

(0)(2 )m a

(0.5 )(2 )m a a

22 22 1

1 4 2

1

12z zI I m a m a a

21.5m a 21.5m a

Determine Iz by using the parallel axis theorem – do parts 1 and 4 first

Parts 2 and 3 are also equal to one another

22 3

1

3z zI I m a

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Group Problem Solving

2 - 28

Calculate Hx

2

2

3( )

23

(0.06211)(0.66667) (8 )21.04067 lb s ft

B x xzH I m a

2

2

3( )

23

(0.06211)(0.66667) (8 )21.04067 lb s ft

B y yzH I m a

2

2

10( )

310

(0.06211)(0.66667) (8 )3

2.3126 lb s ft

B z zH I m a

(1.041 lb ft s) (1.041 lb ft s) (2.31 lb ft s)B H i j k

Calculate Hy

Calculate Hz

Total Vector

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Group Problem Solving

2 - 29

2 2 2 21 1 1 1

2 2 2 2x x y y z z xy x y xz x z yz y z zT I I I I I I I

2 2 2 21 10 1 10(0.06211)(0.66667) (8 )

2 3 2 3T m a

29.1 ft lbT

Calculate the kinetic energy T

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2 - 30

Retracting the landing gear while the wheels are still spinning can result in unforeseen moments being applied to the gear.

When turning a motorcycle, you must “steer” in the opposite direction as you lean into the turn.

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Motion About a Fixed Point or a Fixed Axis

18 - 31

• For a rigid body rotation around a fixed point,

OOxyzO

OO

HH

HM

• For a rigid body rotation around a fixed axis, zzyzyxzx IHIHIH

2

iIjIkIjIiI

kIjIiIk

kIjIiI

HHM

yzxzzyzxz

zyzxz

zyzxz

OOxyzOO

zz

xzyzy

yzxzx

IM

IIM

IIM

2

2

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Rotation About a Fixed Axis

18 - 32

zz

xzyzy

yzxzx

IM

IIM

IIM

2

2• For a rigid body rotation around a fixed axis,

• If symmetrical with respect to the xy plane,

zzyx IMMM 00

• If not symmetrical, the sum of external moments will not be zero, even if = 0,

022 zxzyyzx MIMIM

• A rotating shaft requires both static and dynamic balancing to avoid excessive vibration and bearing reactions.

0 0

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Concept Question

2 - 33

The device at the right rotates about the x axis with a non-constant angular velocity. Which of the following is true (choose one)?

a) You can use Euler’s equations for the provided x, y, z axes

b) The only non-zero moment will be about the x axis

c) At the instant shown, there will be a non-zero y-axis bearing force

d) The mass moment of inertia Ixx is zero

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Sample Problem 18.3

18 - 34

Rod AB with weight W = 40 lb is pinned at A to a vertical axle which rotates with constant angular velocity = 15 rad/s. The rod position is maintained by a horizontal wire BC.

Determine the tension in the wire and the reaction at A.

• Expressing that the system of external forces is equivalent to the system of effective forces, write vector expressions for the sum of moments about A and the summation of forces.

• Solve for the wire tension and the reactions at A.

SOLUTION:

• Evaluate the system of effective forces by reducing them to a vector attached at G and couple

am

.GH

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Sample Problem 18.3

18 - 35

SOLUTION:

• Evaluate the system of effective forces by reducing them to a vector attached at G and coupleam

.GH

I

ILIraa n

2

2212

sft450

cos

Ig

am

lb55945040

kIjIiIH zzyyxxG

0sincos

0 2212

21

zyx

zyx mLIImLI

imLHG

cos2121

kkmL

imLji

HHH GGxyzGG

ftlb645cossin

cossincos0

22121

2121

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Sample Problem 18.3

18 - 36

• Expressing that the system of external forces is equivalent to the system of effective forces, write vector expressions for the sum of moments about A and the summation of forces.

effAA MM

KKT

KIJJIITJ

64519348093.6

64555946.340293.6

lb384T

effFF

IJIKAJAIA ZYX

55940384

JIA

lb 40lb 175

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Group Problem Solving

18 - 37

A four-bladed airplane propeller has a mass of 160 kg and a radius of gyration of 800 mm. Knowing that the propeller rotates at 1600 rpm as the airplane is traveling in a circular path of 600-m radius at 540 km/h, determine the magnitude of the couple exerted by the propeller on its shaft due to the rotation of the airplane

• Determine the mass moment of inertia for the propeller

• Calculate the angular momentum of the propeller about its CG

SOLUTION:

• Determine the overall angular velocity of the aircraft propeller

• Calculate the time rate of change of the angular momentum of the propeller about its CG

• Calculate the moment that must be applied to the propeller and the resulting moment that is applied on the shaft

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Group Problem Solving

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Establish axes for the rotations of the aircraft propeller

Determine the x-component of its angular velocity

540 km/h 150 m/sv

2 rad1600 rpm

60 s

167.55 rad/s

x

150 m/s0.25 rad/s

600 myv

Determine the y-component of its angular velocity

Determine the mass moment of inertia

2 2 2(160 kg)(0.8 m) 102.4 kg mxI mk

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Group Problem Solving

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Angular momentum about G equation:

Determine the couple that is exerted on the shaft by the propeller

Determine the moment that must be applied to the propeller shaft

G x x y yI I H i j

( ) 0 ( )G G Gxyz G y x x y yI I H H Ω H j i j

2(102.4 kg m )(167.55 rad/s)(0.25 rad/s)G x x yI H k k

(4289 N m) = (4.29 kN m)G H k k

Time rate of change of angular momentum about G :

(4.29 kN m)G M H k

(4.29 kN m)on shaft M M k

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Concept Question

2 - 40

The airplane propeller has a constant angular velocity +x. The plane begins to pitch up at a constant angular velocity x

y

zThe propeller has zero angular acceleration

TRUE FALSE

Which direction will the pilot have to steer to counteract the moment applied to the propeller shaft?

a) +x b) +y c) +z

d) -y e) -z

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2 - 41

Gyroscopes are used in the navigation system of the Hubble telescope, and can also be used as sensors (such as in the Segway PT). Modern gyroscopes can also be MEMS (Micro Electro-Mechanical System) devices, or based on fiber optic technology.

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Motion of a Gyroscope. Eulerian Angles

18 - 42

• A gyroscope consists of a rotor with its mass center fixed in space but which can spin freely about its geometric axis and assume any orientation.

• From a reference position with gimbals and a reference diameter of the rotor aligned, the gyroscope may be brought to any orientation through a succession of three steps:

a) rotation of outer gimbal through j about AA’,

b) rotation of inner gimbal through q about

c) rotation of the rotor through y about CC’.

• and are called the Eulerian Angles and

spin of rate

nutation of rate

precession of rate

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Motion of a Gyroscope. Eulerian Angles

18 - 43

• The angular velocity of the gyroscope,

kjK

kji

jiK

cossin

cossinwith

• Equation of motion,

OOxyzOO HHM

jK

kIjIiIHO

cossin

cos

cossincossin

coscos2sin2

dt

dIM

IIM

IIM

z

y

x

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Steady Precession of a Gyroscope

18 - 44

Steady precession,

constant are ,,

ki

kIiIH

ki

zO

z

cossin

sin

sin

jII

HM

z

OO

sincos

Couple is applied about an axis perpendicular to the precession and spin axes

When the precession and spin axis are at a right angle,

jIM O

90

Gyroscope will precess about an axis perpendicular to both the spin axis and couple axis.

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Motion of an Axisymmetrical Body Under No Force

18 - 45

• Consider motion about its mass center of an axisymmetrical body under no force but its own weight, e.g., projectiles, satellites, and space craft.

constant 0 GG HH

• Define the Z axis to be aligned with and z in a rotating axes system along the axis of symmetry. The x axis is chosen to lie in the Zz plane.

GH

xGx IHH sinI

HGx

sin

yy IH 0 0y

zGz IHH cosI

HGz

cos

• = constant and body is in steady precession.

• Note:

tantanI

I

z

x

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Motion of an Axisymmetrical Body Under No Force

18 - 46

Two cases of motion of an axisymmetrical body which under no force which involve no precession:

• Body set to spin about its axis of symmetry,

aligned are and

0

G

xx

H

H

and body keeps spinning about its axis of symmetry.

• Body is set to spin about its transverse axis,

aligned are and

0

G

zz

H

H

and body keeps spinning about the given transverse axis.

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Motion of an Axisymmetrical Body Under No Force

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The motion of a body about a fixed point (or its mass center) can be represented by the motion of a body cone rolling on a space cone. In the case of steady precession the two cones are circular.

• I < I’. Case of an elongated body. and the vector lies inside the angle ZGz. The space cone and body cone are tangent externally; the spin and precession are both counterclockwise from the positive z axis. The precession is said to be direct.

• I > I’. Case of a flattened body. and the vector lies outside the angle ZGz. The space cone is inside the body cone; the spin and precession have opposite senses. The precession is said to be retrograde.

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Concept Question

2 - 48

The rotor of the gyroscope shown to the right rotates with a constant angular velocity. If you hang a weight on the gimbal as shown, what will happen?

a) It will precess around to the right

b) Nothing – it will be in equilibrium

c) It will precess around to the left

d) It will tilt down so the rotor is horizontal