1E10 Lecture in Design Mechanical & Manufacturing Engineering

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Dr. Gareth J. Bennett Trinity College Dublin Page 1 1E10 Lecture in Design 1E10 Lecture in Design Mechanical & Manufacturing Engineering Mechanical & Manufacturing Engineering Dynamics for the Mangonel”. Dr. Gareth J. Bennett

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1E10 Lecture in Design Mechanical & Manufacturing Engineering. “Dynamics for the Mangonel”. Dr. Gareth J. Bennett. Objective. A small model Mangonel. Objective. Can we predict the distance?. Objective. A larger version!. Objective. - PowerPoint PPT Presentation

Transcript of 1E10 Lecture in Design Mechanical & Manufacturing Engineering

Page 1: 1E10 Lecture in Design Mechanical & Manufacturing Engineering

Dr. Gareth J. BennettTrinity College Dublin

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1E10 Lecture in Design1E10 Lecture in DesignMechanical & Manufacturing EngineeringMechanical & Manufacturing Engineering

“Dynamics for the Mangonel”. Dr. Gareth J. Bennett

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Dr. Gareth J. BennettTrinity College Dublin

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ObjectiveObjective

A small model Mangonel

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Dr. Gareth J. BennettTrinity College Dublin

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ObjectiveObjective

Can we predict the distance?

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Dr. Gareth J. BennettTrinity College Dublin

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ObjectiveObjective

A larger version!

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Dr. Gareth J. BennettTrinity College Dublin

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ObjectiveObjective

What are the factors that control the distance? (The dynamics)

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Dr. Gareth J. BennettTrinity College Dublin

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ModellingModelling

Bigger means further?Some of the issues related to

scaling up are discussed in Prof. Fitzpatrick’s lecture!

(Reflect on these)

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Dr. Gareth J. BennettTrinity College Dublin

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ModellingModelling

For a given “size”, can we maximise the distance?What are the key parameters that control the distance?Can we formulate a model that will help us design our Mangonel?

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Dr. Gareth J. BennettTrinity College Dublin

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FundamentalsFundamentals

force = mass x acceleration (ma)

work = force x distance (Fs) energy== work power = rate of work

(work/time)

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Dr. Gareth J. BennettTrinity College Dublin

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Derived Units

Force (1N=1kgm/s2) Work (1J=1Nm=1kgm2/s2) Energy (J) Power (1W=1J/s)

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Starting with some basic equations

Speedav=distance/time

Accelerationav=velocity/time

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Can derive equations for linear motion (for constant acceleration)

v=u+ats=ut+1/2at2

v2=u2+2as

u=initial velocity

v=final velocity

t=time duration

a=acceleration

s=distance travelled

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Example 1: (1-D)Kick a ball straight up. Given

a given initial velocity, how high will it go?

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Example 1: (1-D)

Use equation:v2=u2+2as

s=u2/2g

a=-g

u

v=0 (at top)

s=?

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Example 2: (1-D)Drop a rock from a cliff. How

long will it take to hit the ground/sea?

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Example 2: (1-D)

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Example 2: (1-D)

Use equation:s=ut+1/2at2

s=1/2at2

t (from stopwatch)

u=0 (at top)

s=?

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Example 2: (1-D)

s=1/2at2

t (from stopwatch)

u=0 (at top)

s=?

Example Result: t=3s =>s=44m

However!

t=2.5s =>s=31m

t=3.5s =>s=60m

Sensitive to error: proportional to square of t!

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Can we use these equations to model the trajectory of the missile?

And hence predict the distance?A 2-D problem!

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

y

x

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

y

x

Discretise the curve

1

2

3 4

s

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

y

x

Not u and v now but

v1, v2, v3, v4, etc…..

1

2

3 4

v1

v2

v3v4

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

y

x

We can decompose vectors (v, s, a) into x, y components

1

2

3 4

s1x

s1s1y

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

v=u+at becomes:

•vx2=vx1+ax1Δt

•vy2=vy1+ay1Δt

s=ut+1/2at2 becomes:

•Δsx=vx1Δt+1/2ax1Δt2

•Δsy=vy1Δt+1/2ay1Δt2

Acceleration is constant (for no drag of lift – we’ll return to this point later)

ax=0!

ay=-g

t2-t1= Δt (keep time interval constant)

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics – Assignment1

Use Excel to study trajectory of missile

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01theta (degrees) 30.00theta (radians) 0.52

Input Data

Initial Conditions

vx=Vel*cos(theta)

vy=Vel*sin(theta)

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01theta (degrees) 30.00theta (radians) 0.52

Input Data

Initial Conditions

vx=Vel*cos(theta)

vy=Vel*sin(theta)

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

t2=t1+

Δt

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

x2=x1+vx1Δt+1/2ax1Δt2

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

y2=y1+vy1Δt+1/2ay1Δt2

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

vx2=vx1+ax1Δt

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

vy2=vy1+ay1Δt

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Const=0!

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Const=-g

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00theta (radians) 0.52

Input Data

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Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Copy formula down

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00 3.00 0.02 0.17 0.10 8.66 4.80 0.00 -9.81theta (radians) 0.52 4.00 0.03 0.26 0.15 8.66 4.70 0.00 -9.81

5.00 0.04 0.35 0.19 8.66 4.61 0.00 -9.816.00 0.05 0.43 0.24 8.66 4.51 0.00 -9.817.00 0.06 0.52 0.28 8.66 4.41 0.00 -9.818.00 0.07 0.61 0.33 8.66 4.31 0.00 -9.819.00 0.08 0.69 0.37 8.66 4.21 0.00 -9.81

10.00 0.09 0.78 0.41 8.66 4.11 0.00 -9.8111.00 0.10 0.87 0.45 8.66 4.02 0.00 -9.8112.00 0.11 0.95 0.49 8.66 3.92 0.00 -9.8113.00 0.12 1.04 0.53 8.66 3.82 0.00 -9.8114.00 0.13 1.13 0.57 8.66 3.72 0.00 -9.8115.00 0.14 1.21 0.60 8.66 3.62 0.00 -9.8116.00 0.15 1.30 0.64 8.66 3.53 0.00 -9.8117.00 0.16 1.39 0.67 8.66 3.43 0.00 -9.8118.00 0.17 1.47 0.71 8.66 3.33 0.00 -9.8119.00 0.18 1.56 0.74 8.66 3.23 0.00 -9.81

Input Data

Page 33: 1E10 Lecture in Design Mechanical & Manufacturing Engineering

Dr. Gareth J. BennettTrinity College Dublin

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Dynamics

Plot x versus y using chart wizard

Position t x y vx vy ax ayVel 10.00 1.00 0.00 0.00 0.00 8.66 5.00 0.00 -9.81delt t 0.01 2.00 0.01 0.09 0.05 8.66 4.90 0.00 -9.81theta (degrees) 30.00 3.00 30.01 0.17 0.10 8.66 4.80 0.00 -9.81theta (radians) 0.52 4.00 30.53 0.26 0.15 8.66 4.70 0.00 -9.81

5.00 30.53 0.35 0.19 8.66 4.61 0.00 -9.816.00 30.53 0.43 0.24 8.66 4.51 0.00 -9.817.00 30.53 0.52 0.28 8.66 4.41 0.00 -9.818.00 30.53 0.61 0.33 8.66 4.31 0.00 -9.819.00 30.53 0.69 0.37 8.66 4.21 0.00 -9.81

10.00 30.53 0.78 0.41 8.66 4.11 0.00 -9.8111.00 30.53 0.87 0.45 8.66 4.02 0.00 -9.8112.00 30.53 0.95 0.49 8.66 3.92 0.00 -9.8113.00 30.53 1.04 0.53 8.66 3.82 0.00 -9.8114.00 30.53 1.13 0.57 8.66 3.72 0.00 -9.8115.00 30.53 1.21 0.60 8.66 3.62 0.00 -9.8116.00 30.53 1.30 0.64 8.66 3.53 0.00 -9.8117.00 30.53 1.39 0.67 8.66 3.43 0.00 -9.8118.00 30.53 1.47 0.71 8.66 3.33 0.00 -9.8119.00 30.53 1.56 0.74 8.66 3.23 0.00 -9.8120.00 30.53 1.65 0.77 8.66 3.13 0.00 -9.8121.00 30.53 1.73 0.80 8.66 3.04 0.00 -9.8122.00 30.53 1.82 0.83 8.66 2.94 0.00 -9.81

Input Data

0.00

0.20

0.40

0.60

0.80

1.00

1.20

1.40

0.00 2.00 4.00 6.00 8.00 10.00

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Dr. Gareth J. BennettTrinity College Dublin

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Assignment 1

Mangonel Dynamics Design Tool using Excel

Work in groups and/or individually in computer rooms today and during week to

1.Create excel spreadsheet as demonstrated

2.Plot x versus y

3.Study effect of changing velocity

4.Study effect of changing angle

An assignment will be set based on this work. Assignment to be submitted individually – no copying!