27
G. Leng, ME Dept, NUS 1. Aerodynamics and Firepower or how to “slug” the enemy from a distance

Lecture 1 : Aerodynamics and firepower

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G. L

eng,

ME

Dep

t, N

US

1. A

erod

ynam

ics a

nd F

irep

ower

or h

ow to

“sl

ug”

the

enem

y fr

om a

dis

tanc

e

G. L

eng,

ME

Dep

t, N

US

Quo

tabl

e Q

uote

Cpt

Lidd

ell-H

art*

“It i

s the

fire

pow

er, a

nd fi

re p

ower

alo

ne,

that

arr

ives

at t

he c

orre

ct ti

me

and

plac

e th

at c

ount

s in

the

mod

ern

war

* Si

r Bas

il H

enry

Lid

dell-

Har

t (31

Oct

189

5–29

Jan

1970

) En

glis

hm

ilita

ry h

isto

rian

know

n fo

r his

idea

s on

arm

oure

dw

arfa

rean

d st

rate

gic

theo

ry

G. L

eng,

ME

Dep

t, N

US

Stal

in –

“Art

iller

y is

the

God

of W

ar”

•U

SSR

-V

ladi

mir

Tria

ndaf

ilov

(192

9),

“Cha

ract

er o

f the

Ope

ratio

ns

of M

oder

n Ar

mie

s” e

stim

ated

th

at 5

0-60

gun

s/km

of f

ront

ne

eded

for b

reak

dow

n of

en

emy

defe

nses

.

•W

W2

(194

4) R

ussi

an a

rmie

s us

ed 2

00-3

00 g

uns/

km o

f fr

ont f

or 2

hr b

arra

ge

Ref

: W

alte

r S. D

unn

Jr, “

Hitl

er’s

Nem

esis

: Th

e R

ed A

rmy,

193

0-19

45”,

Pra

eger

, 199

4

G. L

eng,

ME

Dep

t, N

US

Fire

pow

er

The

rate

of e

nerg

yde

liver

edfr

om p

oint

A to

poi

nt B

fo

r des

truc

tive

purp

oses

Que

stio

n : S

o ho

w m

uch

ener

gy c

an b

e de

liver

ed b

y m

oder

n w

eapo

n sy

stem

s ?

G. L

eng,

ME

Dep

t, N

US

Exa

mpl

e : F

H20

00 F

ield

How

itzer

G. L

eng,

ME

Dep

t, N

US

Exa

mpl

e : P

rim

us S

elf P

rope

lled

Art

iller

y

G. L

eng,

ME

Dep

t, N

US

Exa

mpl

e : M

107

155m

m P

roje

ctile

Wei

ght

Leng

th (e

xclu

ding

fuze

)60

5.3

mm

B

ody

diam

eter

154.

89 m

m

Driv

ing

band

dia

met

er15

7.98

mm

Payl

oad

: C

ompo

sitio

n B

: 6.

985

kgTN

T :

6.62

kg

Supp

lem

enta

ry c

harg

e :

0.13

6 kg

TN

T

Rang

e

G. L

eng,

ME

Dep

t, N

US

Exa

mpl

e : X

M98

2 E

xten

ded

Ran

ge A

mm

o•

Join

t dev

elop

men

t by

Bof

ors&

Ray

theo

n

•B

ased

on

stan

dard

155

mm

pro

ject

ile

•C

anar

ds a

erod

ynam

ic c

ontro

ls

•G

PS/IN

S un

it

•C

EP*

= 10

m ra

dius

at a

dis

tanc

e of

50k

m

G. L

eng,

ME

Dep

t, N

US

Ene

rgy

of a

155

mm

HE

pro

ject

ile

Con

side

r the

kin

etic

ene

rgy

for t

he 1

75m

m R

omac

hSP

K.E

.= = =

Ass

umin

g a

payl

oad

frac

tion

of

The

chem

ical

ene

rgy

=

Tota

l ene

rgy

G. L

eng,

ME

Dep

t, N

US

Ene

rgy

of a

GPM

G c

artr

idge

Car

trid

ge, 7

.62m

m, A

P, M

61

Wei

ght(

cartr

idge

) :

Wei

ght (

proj

ectil

e):

M60

mac

hine

gun

Max

eff

ectiv

e ra

nge

Muz

zle

velo

city

: R

ates

of f

ire:

G. L

eng,

ME

Dep

t, N

US

Ene

rgy

of a

GPM

G c

artr

idge

Con

side

r the

kin

etic

ene

rgy

for a

7.6

2mm

M61

AP

proj

ectil

e

K.E

.= = =

Sust

aine

d ra

te o

f fire

is

Muz

zle

“pow

er”

= =

G. L

eng,

ME

Dep

t, N

US

Gal

ileiG

alile

o (1

564-

1642

)

•D

ialo

gues

Con

cern

ing

Two

New

Sci

ence

s–

“ A

proj

ectil

e w

hich

is c

arri

ed b

y a

unifo

rm h

oriz

onta

l m

otio

n co

mpo

unde

d w

ith a

nat

ural

ly a

ccel

erat

ed v

ertic

al

mot

ion

desc

ribe

s a p

ath

whi

ch is

a se

mi-p

arab

ola.

G. L

eng,

ME

Dep

t, N

US

Art

iller

y Pr

ojec

tile

Tra

ject

ory

G. L

eng,

ME

Dep

t, N

US

Fact

ors a

ffec

ting

a re

al tr

ajec

tory

or w

hat G

alile

o di

dn’t

cons

ider

•A

ir re

sist

ance

-ae

rody

nam

ic d

rag

•A

ir di

stur

banc

es –

cros

s win

d, g

ust

•V

aria

ble

atm

osph

eric

pro

perti

es w

ith a

ltitu

de

•D

rift c

ause

d by

pro

ject

ile sp

in

•Ea

rth’s

rota

tion

G. L

eng,

ME

Dep

t, N

US

Bal

listic

coe

ffic

ient

-a

mea

sure

of a

ir r

esis

tanc

e

C=

m/A

=

sect

iona

l den

sity

Cd

form

fact

or

C :

ba

llist

ic c

oeff

icie

nt

m :

m

ass o

f pro

ject

ileA

: cr

oss-

sect

iona

l are

a of

pro

ject

ileC

d:

drag

coe

ffic

ient

(ai

r res

ista

nce)

Not

e : t

he b

allis

tic “

coef

ficie

nt”

has u

nits

of k

g/m

2

G. L

eng,

ME

Dep

t, N

US

Bal

listic

coe

ffic

ient

of 1

55m

m H

E p

roje

ctile

For t

he M

107

155m

m H

E pr

ojec

tile

mas

s =

diam

eter

=

C

d(e

stim

ated

)=

The

balli

stic

coe

ffic

ient

= =

G. L

eng,

ME

Dep

t, N

US

Bal

listic

coe

ffic

ient

of a

bul

let

In S

.I. u

nits

, bal

listic

coe

ffic

ient

= =

G. L

eng,

ME

Dep

t, N

US

Eff

ect o

f air

res

ista

nce

Sim

ulat

ed 1

55m

m H

E tra

ject

ory

Traj

ecto

ry p

aram

eter

s for

max

rang

e

elev

atio

n :

25 d

egra

nge

: 17

.5 k

mtim

e of

flig

ht :

51 s

max

ord

inat

e :

≈3.

5 km

G. L

eng,

ME

Dep

t, N

US

Wor

k ag

ains

t air

res

ista

nce

-los

s of k

inet

ic e

nerg

y

time

s

| V |

m/s

G. L

eng,

ME

Dep

t, N

US

Com

pari

son

: 88m

m P

ak43

Ant

i Tan

k G

un

Muz

zle

velo

city

:

AP

proj

ectil

e:

Pene

tratio

n

:

G. L

eng,

ME

Dep

t, N

US

Sim

ulat

ed 8

8mm

Arm

our

Pier

cing

(AP)

traj

ecto

ry

Traj

ecto

ry p

aram

eter

s (C

D=

0.25

)

elev

atio

n :

0.65

deg

rang

e :

2 50

0mm

ax o

rdin

ate

: ≈

8 m

time

of fl

ight

: 2.

5 s

G. L

eng,

ME

Dep

t, N

US

Com

pari

son

: E

nerg

y lo

ss a

gain

st a

ir r

esis

tanc

e

| V |

m/s

time

s

KE

of A

P pr

ojec

tile

at im

pact

= =

G. L

eng,

ME

Dep

t, N

US

Spin

ning

of a

rtill

ery

proj

ectil

es•

Spin

ning

= f

light

stab

ility

•A

chie

ved

by a

rifle

d ba

rrel

and

co

rres

pond

ing

rota

ting

band

on

proj

ectil

e

•Ex

ampl

e –

155m

m h

owitz

er–

Rifl

ing

of g

un b

arre

l

Cor

resp

ondi

ng ro

tatin

g ba

nd

G. L

eng,

ME

Dep

t, N

US

Aer

odyn

amic

con

sequ

ence

s of s

pinn

ing

The

Mag

nus e

ffect

*

* G

. Mag

nus ,

“On

the

devi

atio

n of

pro

ject

iles;

and

on

a re

mar

kabl

e ph

enom

enon

of r

otat

ing

bodi

es."

, M

emoi

rs o

f the

Roy

al A

cade

my,

Ber

lin,

1852

.

G. L

eng,

ME

Dep

t, N

US

Spin

ning

and

shel

l dri

ft

V

g

G. L

eng,

ME

Dep

t, N

US

Poin

t to

Pond

er

Seas

oned

old

gun

ner :

“ Sh

ell d

rift i

s alw

ays t

o th

e le

ft “

G. L

eng,

ME

Dep

t, N

US

App

licat

ion

exam

ple