a users’ manual and tutorial for performing comet structural

60
NASA Contractor Report 201653 A Users’ Manual and Tutorial for Performing COMET Structural Analyses Using an Advanced User-Friendly Interface Charles L. Blackburn, Christine G. Lotts, and Brian H. Mason Analytical Services and Materials, Inc., Hampton, Virginia Contract NAS1-19700 January 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001

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Page 1: A Users’ Manual and Tutorial for Performing COMET Structural

NASA Contractor Report 201653

A Users’ Manual and Tutorial for Performing COMET Structural Analyses Using an Advanced User-Friendly Interface

Charles L. Blackburn, Christine G. Lotts, and Brian H. MasonAnalytical Services and Materials, Inc., Hampton, Virginia

Contract NAS1-19700

January 1997

National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001

Page 2: A Users’ Manual and Tutorial for Performing COMET Structural

1

AC

E

A dv

ance

d

C

OM

ET

-Int

erfa

ce

E nv

iron

men

t

A U

SER

S' M

AN

UA

L A

ND

TU

TO

RIA

L F

OR

PE

RFO

RM

ING

CO

ME

T S

TR

UC

TU

RA

L A

NA

LY

SES

USI

NG

AN

AD

VA

NC

ED

USE

R-F

RIE

ND

LY

IN

TE

RFA

CE

Cha

rles

L. B

lack

burn

, Chr

istin

e G

. Lot

ts a

nd B

rian

H. M

ason

Ana

lytic

al S

ervi

ces

and

Mat

eria

ls, I

nc.

Ham

pton

, VA

A r

epor

t pre

pare

d fo

r th

e

Com

puta

tiona

l Mec

hani

cs B

ranc

h

NA

SA L

angl

ey R

esea

rch

Cen

ter

Fore

wor

d

Thi

s us

ers'

man

ual

desc

ribe

s th

e us

e of

a g

raph

ical

inte

rfac

e de

velo

ped

for

the

gene

ral p

urpo

se f

inite

ele

men

t sys

tem

, CO

ME

T.

The

re h

as b

een

som

e co

nsid

erat

ions

giv

en to

use

r-fr

iend

ly c

once

rns

in th

is d

evel

opm

ent a

nd th

ese

cons

ider

atio

ns w

ill c

ontin

ue a

nd

incr

ease

in p

rior

ity a

s th

e co

mpl

exity

of

the

anal

yses

incr

ease

s. W

hen

the

inte

rfac

e is

ful

ly u

ser-

frie

ndly

, it

will

not

be

nece

ssar

y to

wri

te t

his

user

s' m

anua

l.

Page 3: A Users’ Manual and Tutorial for Performing COMET Structural

2 Intr

oduc

tion

The

CO

ME

T s

oftw

are

syst

em is

a h

ighl

y m

odul

ar a

nd f

lexi

ble

stru

ctur

al a

naly

sis

syst

em f

or r

esea

rch

in c

ompu

tatio

nal m

etho

ds

and

for

expl

orat

ion

of n

ew m

ultip

roce

ssor

and

vec

tor

com

pute

r ha

rdw

are.

The

se a

ttrib

utes

: nam

ely,

mod

ular

ity a

nd f

lexi

bilit

y, m

ake

CO

ME

T a

ttrac

tive

to a

naly

sts,

res

earc

hers

, and

dev

elop

ers

in th

e st

ruct

ural

mec

hani

cs d

isci

plin

e. H

owev

er, t

hese

attr

ibut

es c

ontr

ibut

e to

the

com

plex

ity o

f th

e sy

stem

and

mak

e its

usa

ge d

iffi

cult

to g

rasp

. A

lthou

gh th

e en

gine

er/u

ser

who

wan

ts to

per

form

an

anal

ysis

may

unde

rsta

nd th

e da

ta r

equi

rem

ents

and

mat

hem

atic

al m

anip

ulat

ions

req

uire

d to

eff

ect h

is/h

er d

esir

ed r

esul

ts, h

e/sh

e m

ay n

ot b

e ab

le to

,

•id

entif

y th

e pr

oced

ures

and

/or

proc

esso

rs r

equi

red

for

a pa

rtic

ular

ana

lysi

s an

d th

eir

rela

ted

I/O

req

uire

men

ts a

nd

•in

tera

ct w

ith th

e co

mpu

ter

to e

xecu

te C

OM

ET

with

out e

xten

sive

trai

ning

, or

by r

eadi

ng a

pplic

able

doc

umen

tatio

n an

d/or

atte

ndin

g

clas

ses.

Con

sequ

ently

, a v

alua

ble

tool

is lo

st to

the

gene

ric

user

who

may

be

unw

illin

g or

una

ble

to a

ffor

d th

e tim

e on

the

lear

ning

cur

ve b

efor

e

they

can

per

form

mea

ning

ful a

naly

ses.

The

refo

re, t

he d

evel

opm

ent o

f a

user

-fri

endl

y in

terf

ace

will

per

mit

imm

edia

te e

xecu

tion

of th

e

prog

ram

by

a no

vice

use

r w

hile

pro

vidi

ng tr

aini

ng th

roug

h an

inte

ract

ive

quer

y m

ode

such

that

the

user

will

bec

ome

prof

icie

nt w

ith th

e

soft

war

e an

d ha

rdw

are.

Thi

s in

itial

dev

elop

men

t has

bee

n di

rect

ed to

war

d th

e ge

neri

c us

er w

ho w

ill b

e pe

rfor

min

g st

ruct

ural

ana

lyse

s on

a co

mpo

nent

or

an a

ssem

bly

of s

truc

tura

l com

pone

nts.

Fut

ure

deve

lopm

ent w

ill e

nhan

ce th

is u

ser-

frie

ndly

inte

rfac

e to

sup

port

the

deve

lopm

ent o

f th

e sy

stem

by

rese

arch

ers

and/

or c

ompu

ter

scie

ntis

ts.

AC

E (

A dv

ance

d

C

OM

ET

-Int

erfa

ce

E nv

iron

men

t) p

rovi

des

the

capa

bilit

y to

cre

ate

and

exec

ute

a C

OM

ET

run

stre

am f

ile b

y

inte

ract

ive

quer

y of

the

user

and

/or

pull

dow

n m

enu

sele

ctio

ns f

or d

efin

ing

the

I/O

and

the

type

of

anal

ysis

. T

wo

mod

es o

f in

tera

ctio

n

have

bee

n im

plem

ente

d; n

amel

y, "

QU

ER

Y"

(or

novi

ce)

and

"EX

PER

T".

Eac

h of

thes

e m

odes

onl

y ad

dres

ses

the

user

s' c

apab

ility

in

exer

cisi

ng th

e C

OM

ET

pro

gram

and

doe

s no

t ref

er to

thei

r ex

pert

ise

in p

erfo

rmin

g fi

nite

ele

men

t ana

lysi

s or

com

pute

r sy

stem

ope

ratio

ns.

In th

e Q

UE

RY

mod

e, th

e ru

nstr

eam

is c

reat

ed b

y qu

eryi

ng th

e us

er a

nd d

irec

ting

them

to th

e pr

oper

men

u se

lect

ions

. In

the

"EX

PER

T"

mod

e, it

is a

ssum

ed th

at th

e us

er is

fam

iliar

with

the

prog

ram

and

the

use

of w

indo

w-b

ased

app

licat

ion

soft

war

e.

Get

ting

Star

ted

The

AC

E d

evel

opm

ent i

s be

ing

done

on

a U

NIX

bas

ed D

EC

Stat

ion

5000

wor

ksta

tion.

The

app

licat

ion

soft

war

e ca

n be

por

ted

to

othe

r U

NIX

bas

ed w

orks

tatio

ns a

nd m

ainf

ram

es w

hich

sup

port

X-w

indo

ws

and

Mot

if.

The

hos

t com

pute

r m

ust h

ave

suff

icie

nt m

emor

y,

Page 4: A Users’ Manual and Tutorial for Performing COMET Structural

3

both

RA

M a

nd h

ard

disk

, to

satis

fy th

e re

quir

emen

ts o

f bo

th A

CE

and

CO

ME

T.

The

use

r ca

n ru

n A

CE

fro

m a

rem

ote

X w

orks

tatio

n su

ch

as a

Mac

into

sh w

ith M

acX

(ve

rsio

n 1.

2 or

hig

her)

or

a U

NIX

bas

ed w

orks

tatio

n w

ith a

n X

win

dow

ser

ver

runn

ing.

Thi

s Ph

ase

1 im

plem

enta

tion

has

been

res

tric

ted

to p

erfo

rmin

g lin

ear

stat

ic a

naly

ses

on s

tiffe

ned

shel

l str

uctu

res

mad

e of

isot

ropi

c

mat

eria

ls.

It is

ass

umed

that

the

geom

etry

(no

des

and

elem

ents

) of

the

fini

te e

lem

ent m

odel

hav

e be

en p

revi

ousl

y de

fine

d by

a P

AT

RA

N

exer

cise

or

have

bee

n st

ored

in a

CO

ME

T d

ata

base

file

. Fu

rthe

r, th

e PA

TR

AN

neu

tral

file

may

con

tain

con

stra

int,

load

s, a

nd e

lem

ent

orie

ntat

ion

data

and

the

CO

ME

T d

ata

base

file

may

con

tain

all

the

abov

e in

add

ition

to m

ater

ial a

nd s

ectio

n pr

oper

ty d

ata.

The

se f

iles

mus

t exi

st o

n th

e sa

me

com

pute

r w

here

AC

E is

bei

ng e

xecu

ted.

Setu

p W

orks

tatio

n to

Exe

cute

AC

E

AC

E is

exe

cute

d on

a U

NIX

hos

t com

pute

r w

here

CO

ME

T a

lso

resi

des.

It's

win

dow

s ar

e di

spla

yed

on a

rem

ote

X W

indo

w

wor

ksta

tion.

It c

an b

e in

itiat

ed in

one

of

two

way

s. T

he f

irst

way

is to

log

in to

the

host

com

pute

r w

ith th

e "t

elne

t" o

r "r

logi

n" c

omm

and

in a

n xt

erm

win

dow

, the

n on

ce lo

gged

in, e

xecu

te A

CE

with

the

"run

_ace

" co

mm

and.

The

sec

ond

way

is to

exe

cute

a r

emot

e sh

ell t

o th

e

host

com

pute

r, f

or e

xam

ple:

rsh blackbird "setenv DISPLAY workstation:0.0; /usr/bin/X11/xterm -ls -e /csm/bin/run_ace working_directory"

whe

re workstation:0.0

sho

uld

be th

e ne

twor

k ad

dres

s an

d sc

reen

of

your

wor

ksta

tion'

s X

-ser

ver.

The

working_directory

para

met

er s

houl

d be

the

nam

e of

the

dire

ctor

y yo

u w

ant t

o w

ork

in o

n th

e ho

st c

ompu

ter;

it c

an b

e om

itted

if y

ou w

ant t

o w

ork

in y

our

hom

e di

rect

ory.

On

a M

acin

tosh

wor

ksta

tion

runn

ing

Mac

X v

ersi

on 1

.2, y

ou c

an s

et u

p th

e co

mm

and

to b

e ex

ecut

ed o

n bl

ackb

ird

as f

ollo

ws:

setenv DISPLAY "workstation:0.0"; /usr/bin/X11/xterm -ls -e /csm/bin/run_ace "working_directory"

Page 5: A Users’ Manual and Tutorial for Performing COMET Structural

4

whe

re "workstation:0.0" i

s th

e ne

twor

k ad

dres

s a

nd s

cree

n of

you

r w

orks

tatio

n's

X-s

erve

r. Y

ou c

an s

ubst

itute

"®display"

is ty

ped

by h

oldi

ng d

own

the

optio

n ke

y an

d st

riki

ng th

e r-

key)

in p

lace

of

"workstation:0.0"

and

Mac

X w

ill p

lace

the

corr

ect

info

rmat

ion

for

you.

The

"working_directory"

para

met

er s

houl

d be

the

nam

e of

the

dire

ctor

y yo

u w

ant t

o w

ork

in o

n th

e ho

st

com

pute

r; it

can

be

omitt

ed if

you

wan

t to

wor

k in

you

r ho

me

dire

ctor

y .

Sele

ctin

g th

e L

evel

of

Inte

ract

ion

As

men

tione

d ea

rlie

r, A

CE

can

be

run

in tw

o m

odes

of

inte

ract

ion,

"Q

UE

RY

" or

"E

XPE

RT

". T

o be

gin

exec

utio

n of

AC

E, t

ype

run_

ace

-e

C/R

to

exe

cute

AC

E in

the

"EX

PER

T"

mod

e

run_

ace

-q

C/R

to

exe

cute

AC

E in

the

"QU

ER

Y"

(def

ault)

mod

e

whi

ch th

en b

ring

s up

the

AC

E m

ain

win

dow

, sho

wn

in F

igur

e 1.

Page 6: A Users’ Manual and Tutorial for Performing COMET Structural

5

Mai

n M

enu

Bar

Stat

us B

ar"r

adio

" B

utto

ns

Fig

ure

1

•T

he h

oriz

onta

l bar

whi

ch s

pans

the

wid

th o

f th

e m

ain

win

dow

is th

e

m

enu

bar

with

pul

l-do

wn

men

us f

or f

requ

ently

use

d fu

nctio

ns.

•T

he in

term

edia

te r

egio

n be

low

the

men

ubar

is th

e co

ntro

l are

a w

ith "

radi

o " b

utto

ns f

or th

e su

b-gr

oups

of

prob

lem

def

initi

on.

•In

the

low

er le

ft c

orne

r of

the

mai

n m

enu

win

dow

, bel

ow th

e co

ntro

l are

a is

an

info

rmat

ion

box,

cal

led

the

"sta

tus

bar"

. T

he m

ode

of

inte

ract

ion,

the

curr

ent d

irec

tory

(in

this

cas

e, w

ork)

whe

re th

e fi

nite

ele

men

t mod

el r

esid

es, t

he n

ame

of th

e m

odel

file

, and

the

type

of a

naly

sis

are

disp

laye

d in

the

stat

us b

ar.

The

"Q

UE

RY

" m

ode

will

giv

e th

e us

er d

etai

led

info

rmat

ion

on h

ow to

pro

ceed

thro

ugh

the

men

us in

a p

re-d

efin

ed s

tep

by s

tep

man

ner

to

form

ulat

e or

mod

ify

and

exec

ute

the

runs

trea

m.

The

"E

XPE

RT

" m

ode

perm

its th

e us

er to

mak

e hi

s/he

r ow

n se

lect

ions

, with

out g

uida

nce,

fro

m th

e to

p-le

vel m

enu

and

cont

rol a

rea.

Page 7: A Users’ Manual and Tutorial for Performing COMET Structural

6

For

the

pres

ent e

xerc

ise,

exe

cute

AC

E in

the

"QU

ER

Y"

mod

e by

ent

erin

g,

run_

ace

-q

C/R

*

* B

old

Let

teri

ng in

dica

tes

a re

spon

se b

y th

e us

er.

Page 8: A Users’ Manual and Tutorial for Performing COMET Structural

7

AC

E R

oad

Map

The

bas

ic p

roce

dure

to b

e pe

rfor

med

in A

CE

is o

utlin

ed in

the

tabl

e ab

ove.

The

ste

ps r

equi

red

for

crea

ting

and

exec

utin

g a

CO

ME

T a

naly

sis

are

liste

d in

the

orde

r th

at th

ey s

houl

d be

per

form

ed, a

nd th

e A

CE

scr

een

com

pone

nts

used

to in

itiat

e th

e ac

tions

are

show

n. D

etai

led

disc

ussi

on o

f th

e sc

reen

s an

d da

ta is

pre

sent

ed la

ter

in th

is r

epor

t.

Fun

ctio

nA

CE

Scr

een

Com

pone

nt

Spec

ify

anal

ysis

type

Men

u B

ar/A

naly

sis

Inpu

t Mod

el g

eom

etry

Men

u B

ar/F

ile/O

pen

Mod

el D

atab

ase

Sele

ct C

OM

ET

ele

men

tsD

efin

e E

lem

ents

Dia

log

Exa

min

e in

itial

mod

el (

optio

nal)

CO

ME

T G

raph

ics

Proc

esso

r M

enus

Def

ine

mat

eria

l pro

pert

ies

Mat

eria

ls "

radi

o" B

utto

n

Def

ine

sect

ion

prop

ertie

sSe

ctio

n Pr

ops.

"ra

dio"

But

ton

Def

ine/

mod

ify

boun

dary

con

ditio

nsB

C "

radi

o" B

utto

n

Sele

ct a

naly

sis

optio

nsM

enu

Bar

/Pre

fere

nces

/Ana

lysi

s

Exe

cute

Exe

cute

"ra

dio"

But

ton

Post

-pro

cess

res

ults

(op

tiona

l)R

esul

ts "

radi

o" B

utto

n

Don

eM

enu

Bar

/Qui

t

Page 9: A Users’ Manual and Tutorial for Performing COMET Structural

8

Fig

ure

2

Sele

ctin

g th

e T

ype

of S

truc

tura

l Ana

lysi

s

T

he s

cree

n w

ill n

ow a

ppea

r as

sho

wn

in F

igur

e 2

with

the

"HE

LP"

win

dow

in

the

uppe

r ri

ght h

and

corn

er w

hich

is th

e us

ual

loca

tion.

•T

he H

EL

P w

indo

w h

as a

whi

te b

ackg

roun

d an

d co

ntai

ns d

etai

led

inst

ruct

ions

.

• I

t is

note

d th

at th

e "Q

UE

RY

" se

lect

ion

has

been

iden

tifie

d in

the

"sta

tus

bar"

.

Aft

er r

eadi

ng th

e op

erat

iona

l ins

truc

tions

for

the

mou

se a

nd d

ata

entr

ies,

the

user

is in

stru

cted

to c

lick

on th

e A

NA

LY

SIS

men

u ite

m

(whi

ch h

as b

een

high

light

ed)

and

then

sel

ect a

n A

NA

LY

SIS

type

. C

lick

on "

AN

AL

YSI

S".

Not

e: O

n oc

casi

ons,

the

"HE

LP"

win

dow

may

be

"low

ered

" be

low

the

mai

n w

indo

w.

Clic

k on

"H

elp"

but

ton

to r

aise

it to

the

top.

Page 10: A Users’ Manual and Tutorial for Performing COMET Structural

9

Fig

ure

3

Whe

n th

e m

ouse

is c

licke

d on

top

of th

e A

NA

LY

SIS

men

u ite

m,

the

sub-

men

u w

indo

w e

ntitl

ed "

AN

AL

YSI

S O

PTIO

NS

ME

NU

"

is o

pene

d as

sho

wn

in F

igur

e 3.

•Se

vera

l ana

lysi

s op

tions

are

list

ed.

•So

me

men

u ite

ms

can

be s

elec

ted

to r

evea

l ano

ther

leve

l of

men

us (

as in

dica

ted

by th

e th

ree

dots

fol

low

ing

the

nam

e of

the

men

u

item

).

•A

ll ite

ms

exce

pt f

or L

INE

AR

ST

AT

IC a

ppea

r gr

ay in

col

or a

s th

ey h

ave

not b

een

impl

emen

ted

as y

et, b

ut a

re p

lann

ed f

or la

ter

rele

ases

.

Clic

k on

"L

inea

r St

atic

" to

spe

cify

the

anal

ysis

type

to b

e us

ed f

or th

is s

essi

on.

Page 11: A Users’ Manual and Tutorial for Performing COMET Structural

10

Fig

ure

4

Sele

ctin

g th

e Fi

nite

Ele

men

t Mod

el F

ile

The

"st

atus

bar

" in

Fig

ure

4 in

dica

tes

the

sele

ctio

n of

"L

inea

r St

atic

" an

alys

is a

nd th

e "H

EL

P" w

indo

w d

irec

ts th

e us

er to

clic

k on

the

FIL

E m

enu

item

(w

hich

is n

ow h

ighl

ight

ed)

to s

elec

t a f

inite

ele

men

t mod

el f

ile th

at c

urre

ntly

exi

sts

on th

is c

ompu

ter

whe

re A

CE

is

bein

g ex

ecut

ed.

Clic

k on

"F

ile".

Page 12: A Users’ Manual and Tutorial for Performing COMET Structural

11

Fig

ure

5

Aft

er c

licki

ng o

n FI

LE

, the

pul

l-do

wn

men

u ca

lled

"FIL

ES

ME

NU

" ap

pear

s as

sho

wn

in F

igur

e 5.

The

gra

y m

enu

item

s ar

e no

t

avai

labl

e fo

r se

lect

ion

at th

is ti

me

eith

er b

ecau

se th

ey a

re n

ot r

equi

red

at th

e pr

esen

t tim

e, o

r th

ey h

ave

not b

een

impl

emen

ted

as y

et.

The

user

has

bee

n in

stru

cted

to s

elec

t a m

odel

file

; the

refo

re, c

lick

on "

Ope

n M

odel

Dat

abas

e".

Thi

s se

lect

ion

will

cau

se a

ll fi

les

with

a "

pat"

(PA

TR

AN

neu

tral

file

s) o

r "d

bc"

(CO

ME

T d

atab

ase

file

s) e

xten

sion

to b

e se

lect

ed f

rom

the

dire

ctor

y id

entif

ied

in th

e "s

tatu

s

bar"

( in

this

exa

mpl

e, t

he d

irec

tory

is "

wor

k").

As

prev

ious

ly m

entio

ned,

the

thre

e (3

) do

ts f

ollo

win

g a

men

u ite

m in

dica

tes

that

ano

ther

leve

l of

inte

ract

ive

user

res

pons

e fo

llow

s.

For

this

exe

rcis

e, th

e pr

evio

us a

ctio

n op

ened

up

the

win

dow

sho

wn

in F

igur

e 6(

a).

•T

he "

HE

LP"

win

dow

ins

truc

ts th

e us

er to

clic

k on

the

"rad

io"

butto

n de

sign

atin

g th

e fi

le ty

pe c

onta

inin

g th

e m

odel

file

.

•T

he d

efau

lt se

lect

ion

is P

AT

RA

N N

eutr

al F

iles.

•C

licki

ng o

n ea

ch d

ispl

ays

a lis

t of

file

s o

f th

e co

rres

pond

ing

type

ava

ilabl

e in

the

wor

king

dir

ecto

ry.

Page 13: A Users’ Manual and Tutorial for Performing COMET Structural

12

•In

the

even

t tha

t the

mod

el f

iles

are

cont

aine

d in

a d

iffe

rent

dir

ecto

ry th

an th

e w

orki

ng d

irec

tory

, the

use

r ca

n na

viga

te th

e fi

le s

yste

m

to th

e de

sire

d di

rect

ory

by c

licki

ng o

n th

e "O

ne L

evel

Abo

ve"

or "

One

Lev

el B

elow

" as

man

y tim

es a

s ar

e re

quir

ed.

•H

avin

g lo

cate

d th

e de

sire

d m

odel

file

(w

hich

may

req

uire

usi

ng th

e sc

roll

bars

if th

ere

are

too

man

y fi

les

to a

ppea

r in

the

win

dow

),

plac

e th

e cu

rsor

on

top

of t

he f

ile (

for

this

exa

mpl

e, "

dem

o1"

or "

dem

o2")

and

clic

k.

•T

his

will

hig

hlig

ht th

e se

lect

ed f

ile n

ame.

T

he f

ile n

ame

is a

lso

disp

laye

d in

the

" Se

lect

ion "

fie

ld b

elow

the

"rad

io"

butto

ns (

Fig.

6

(b))

.

•T

he n

ame

and

iden

tific

atio

n o

f th

e fi

le w

ill a

ppea

r in

the

"HE

LP"

win

dow

(Fi

g. 6

(b)

).

•Y

ou c

an c

hang

e th

e se

lect

ion

by s

crol

ling

thro

ugh

the

list o

f fi

le n

ames

and

sel

ectin

g an

othe

r fi

le b

y pl

acin

g th

e cu

rsor

on

the

file

nam

e an

d cl

icki

ng to

sel

ect.

Clic

king

on

"Can

cel"

cau

ses

the

file

sel

ectio

n pr

oces

s to

term

inat

e w

ithou

t a f

ile b

eing

sel

ecte

d.

Now

, clic

k on

"Se

lect

" to

sel

ect t

he id

entif

ied

file

Page 14: A Users’ Manual and Tutorial for Performing COMET Structural

13

Fig

ure

6 (a

)

Page 15: A Users’ Manual and Tutorial for Performing COMET Structural

14

F

igur

e 6

(b)

Fig

ure

6 (c

)

At t

his

poin

t, a

smal

l "in

fo"

win

dow

, in

the

cent

er o

f th

e sc

reen

, di

rect

s th

e us

er to

wai

t whi

le th

e de

sign

ated

file

is b

eing

proc

esse

d to

ext

ract

the

data

des

crib

ing

the

fini

te e

lem

ent m

odel

. (T

he p

rese

nt P

AT

RA

N p

roce

ssor

doe

s no

t rec

ogni

ze s

ome

load

ing

data

such

a d

istr

ibut

ed lo

ads,

mor

e th

an o

ne lo

ad o

r co

nstr

aint

cas

e, m

ater

ial p

rope

rtie

s, a

nd s

ectio

n pr

oper

ties.

) S

ee A

ppen

dix

A f

or a

disc

ussi

on o

f ho

w th

e ne

utra

l file

dat

a is

ass

ocia

ted

with

CO

ME

T m

odel

ing

capa

bilit

ies.

Page 16: A Users’ Manual and Tutorial for Performing COMET Structural

15

Gen

erat

ing

the

Run

stre

am f

or D

efin

ing

the

Fini

te E

lem

ent M

odel

Ele

men

t Sel

ectio

n

As

show

n in

Fig

ure

7 (a

), th

e "s

tatu

s ba

r" r

efle

cts

the

nam

e of

the

file

sel

ecte

d an

d th

e "H

EL

P" w

indo

w d

escr

ibes

the

step

s to

follo

w in

sel

ectin

g th

e C

OM

ET

ele

men

t for

mul

atio

ns.

The

se s

teps

are

rei

tera

ted

in a

n ab

brev

iate

d fo

rm in

the

"Def

ine

Ele

men

ts"

win

dow

alon

g w

ith th

e na

me

of th

e m

odel

file

in w

hich

the

elem

ent t

ypes

wer

e fo

und.

Sinc

e th

e el

emen

t typ

es a

re p

urel

y a

func

tion

of th

e ge

omet

ry, i

t is

nece

ssar

y to

sel

ect a

n el

emen

t for

mul

atio

n th

at w

ill d

escr

ibe

the

resp

onse

of

a st

ruct

ural

com

pone

nt r

epre

sent

ed b

y th

is f

inite

ele

men

t mod

el.

For

exa

mpl

e, in

som

e si

tuat

ions

a 2

-nod

e ro

d el

emen

t tha

t

carr

ies

an a

xial

load

onl

y m

ay b

e pr

efer

red

over

the

mor

e co

mpl

ex 2

-nod

e be

am th

at c

arri

es a

xial

and

she

ar lo

ads

and

bend

ing

and

tors

iona

l mom

ents

. T

hese

ele

men

t typ

es c

an b

e

(a)

2-no

de b

eam

ele

men

ts,

(b)

3, 4

, and

9-n

ode

plat

e an

d sh

ell e

lem

ents

,

(c)

8, 1

0 an

d 20

-nod

e so

lid e

lem

ents

and

/or

(d)

12 a

nd 1

5-no

de s

hell-

to-s

olid

tran

sitio

n el

emen

ts (

not i

mpl

emen

ted

in th

e cu

rren

t PA

TR

AN

tran

slat

or).

Sele

ct a

n "e

lem

ent

type

" (t

he s

elec

tion

will

be

high

light

ed)

from

the

top

win

dow

. A

list

of

avai

labl

e C

OM

ET

ele

men

ts

corr

espo

ndin

g to

this

nod

al a

rran

gem

ent w

ill a

ppea

r in

the

win

dow

bel

ow th

e "E

lem

ent T

ypes

" (F

ig. 7

(b)

). A

"H

elp"

win

dow

(Fi

g. 7

(c)

)

will

app

ear

in th

e us

ual l

ocat

ion.

Clic

king

on

a pa

rtic

ular

ele

men

t will

hig

hlig

ht th

at s

elec

tion

(Fig

. 7 (

d))

and

info

rmat

ion

desc

ribi

ng th

e fo

rmul

atio

n of

the

elem

ent

and

the

reco

mm

ende

d us

e w

ill b

e di

spla

yed

in th

e "E

lem

ent I

nfor

mat

ion"

win

dow

(Fi

g. 7

(f

)) w

hich

is in

the

cent

ral p

art o

f th

e sc

reen

.

As

expl

aine

d in

the

"Hel

p" w

indo

w (

Fig.

7 (

e)),

ano

ther

sel

ectio

n ca

n be

mad

e if

aft

er r

eadi

ng th

is in

form

atio

n yo

u fi

nd th

at th

e el

emen

t

does

not

sat

isfy

you

r m

odel

ing

requ

irem

ents

. (A

t thi

s tim

e, A

CE

can

onl

y ac

com

mod

ate

a si

ngle

ele

men

t for

mul

atio

n fo

r ea

ch e

lem

ent

geom

etry

.)

Onc

e a

CO

ME

T e

lem

ent h

as b

een

sele

cted

for

a p

artic

ular

ele

men

t geo

met

ry, r

etur

n to

the

"Def

ine

Ele

men

ts"

win

dow

(Fi

g. 7

(g)

)

and

cont

inue

to s

peci

fy a

CO

ME

T e

lem

ent f

or a

ll re

mai

ning

ele

men

ts g

eom

etry

fou

nd in

the

mod

el f

ile (

Figs

. 7 (

h) a

nd 7

(i)

) un

til th

e

entir

e lis

t is

exha

uste

d. T

he s

elec

tions

do

not h

ave

to b

e do

ne in

ord

er a

nd c

an b

e ch

ange

d. R

efer

ring

to th

e in

stru

ctio

ns in

the

"Hel

p"

Page 17: A Users’ Manual and Tutorial for Performing COMET Structural

16

win

dow

(Fi

g. 7

(e)

), c

lick

on "

Acc

ept"

. Fi

nally

, the

use

r is

ask

ed to

con

firm

his

/her

ele

men

t sel

ectio

ns o

r re

peat

som

e or

all

of th

e

prio

r st

eps.

Clic

k on

the

app

ropr

iate

but

ton.

Page 18: A Users’ Manual and Tutorial for Performing COMET Structural

17

Fig

ure

7 (a

)

Page 19: A Users’ Manual and Tutorial for Performing COMET Structural

18

Fig

ure

7(b)

Fig

ure

7(c

)

Page 20: A Users’ Manual and Tutorial for Performing COMET Structural

19

Fig

ure

7(d)

Fig

ure

7(e)

Fig

ure

7(f)

Page 21: A Users’ Manual and Tutorial for Performing COMET Structural

20

Fig

ure

7 (g

)

Fig

ure

7 (

h)

Page 22: A Users’ Manual and Tutorial for Performing COMET Structural

21

Fig

ure

7 (i

)

Fig

ure

7 (j

)

Ass

umin

g th

at th

e ne

cess

ary

and

rel

evan

t ele

men

ts h

ave

been

acc

epte

d, t

he u

ser

is a

dvis

ed to

wai

t (se

e Fi

g. 8

) an

d th

en th

e fi

nite

Fig

ure

8

elem

ent

mod

el is

dis

play

ed in

a C

OM

ET

Gra

phic

s (C

Gx)

win

dow

as

show

n in

Fig

ure

9 (a

) al

ong

with

the

"mai

n m

enu"

and

"H

elp"

win

dow

s. T

he C

Gx

win

dow

has

its

own

set o

f m

enus

and

its

gene

ral u

se w

ill n

ot b

e do

cum

ente

d he

rein

. T

he "

Hel

p" w

indo

w i

nfor

ms

the

user

of

the

num

ber

of s

ectio

n ty

pes

that

hav

e be

en id

entif

ied

(one

for

"de

mo1

" an

d tw

o fo

r "d

emo2

") a

nd d

irec

ts th

e us

er to

clic

k on

the

high

light

ed "

Mat

eria

ls"

"rad

io"

butto

n in

the

cont

rol a

rea.

Clic

k on

the

"ra

dio"

but

ton

adja

cent

to

"Mat

eria

ls"

(it w

ill

glow

red

).

Page 23: A Users’ Manual and Tutorial for Performing COMET Structural

22

Mat

eria

l Pro

pert

ies

Def

initi

on

Sele

ctin

g th

e M

ater

ials

"ra

dio"

but

ton

disp

lays

a "

MA

TE

RIA

LS

SEL

EC

TIO

N D

IAL

OG

" w

indo

w, a

long

with

an

upda

ted

"Hel

p"

win

dow

(Fi

g. 9

(b)

). F

ollo

win

g th

e di

rect

ions

giv

en in

the

"Hel

p" w

indo

w,

•T

o se

lect

a m

ater

ial t

ype,

clic

k on

the

"op

tion

" bu

tton

labe

led

"Iso

trop

ic",

the

defa

ult m

ater

ial t

ype.

•A

n op

tion

men

u w

ill a

ppea

r lis

ting

seve

ral m

ater

ial t

ypes

suc

h as

Iso

trop

ic, O

rtho

trop

ic, P

last

icity

, 2-D

Ani

sotr

opic

, 3-D

Ani

sotr

opic

,

and

Com

posi

te.

The

mat

eria

l typ

es s

how

n in

gra

y ha

ve n

ot b

een

impl

emen

ted.

•T

he u

ser

is n

ow a

sked

abo

ut th

e lo

catio

n of

the

mat

eria

ls d

ata.

In

othe

r w

ords

, doe

s th

e da

ta r

esid

e on

a a

rchi

ved

data

base

(av

aila

ble

in th

is w

orki

ng d

irec

tory

) or

mus

t the

dat

a be

ent

ered

usi

ng th

e ke

yboa

rd.

•T

o de

fine

a n

ew m

ater

ial (

whi

ch is

the

defa

ult)

, an

swer

"Y

es"

to th

e se

cond

que

stio

n.

•T

o se

lect

a m

ater

ial f

rom

an

arch

ived

mat

eria

ls d

atab

ase,

clic

k on

the

"ra

dio"

but

ton

next

to

"Yes

" a

fter

the

firs

t que

stio

n.

The

but

ton

will

glo

w r

ed.

The

ans

wer

to "

Def

ine

A N

ew M

ater

ial?

" w

ill a

utom

atic

ally

be

set t

o "N

o".

•A

mod

ifie

d "M

AT

ER

IAL

S SE

LE

CT

ION

DIA

LO

G"

win

dow

(Fi

g. 9

(d)

) th

at a

lso

refl

ects

the

new

hel

p m

essa

ges

is d

ispl

ayed

. T

he

user

is in

stru

cted

to c

lick

on "

File

s" m

enu

and

then

sel

ect

the

"Ope

n M

ater

ial D

atab

ase"

opt

ion

(Fig

. 9 (

e)).

Thi

s ac

tion

open

s th

e "M

ater

ial D

atab

ase

Sele

ctio

n" w

indo

w (

Fig.

9 (

f))

whi

ch li

sts

all t

he m

ater

ial d

atab

ase

file

s (t

hose

with

the

file

exte

nsio

n, "

mat

").

•Se

lect

the

desi

red

mat

eria

ls d

atab

ase

file

by

clic

king

on

the

nam

e of

the

file

("m

ater

ials

.mat

" fo

r th

is e

xam

ple)

. T

he s

elec

tion

is

high

light

ed (

Fig.

9 (

g)).

•T

he n

ames

of

the

mat

eria

ls o

f th

e se

lect

ed m

ater

ial t

ype

avai

labl

e in

the

sele

cted

mat

eria

ls f

ile a

re li

sted

in a

scr

olla

ble

sub-

win

dow

of

the

"MA

TE

RIA

LS

SEL

EC

TIO

N D

IAL

OG

" w

indo

w ti

tled

"Mat

eria

ls in

Dat

abas

e Fi

le:"

(Fi

g 9

(h))

.

•T

o se

lect

a m

ater

ial f

or a

dditi

on to

the

runs

trea

m, p

lace

cur

sor

on t

op o

f th

at m

ater

ial a

nd c

lick.

The

sel

ectio

n w

ill b

e

high

light

ed (

Fig

9 (i

)) a

nd w

ill a

ppea

r im

med

iate

ly in

the

sub-

win

dow

cal

led

"Mat

eria

ls S

elec

ted

For

Com

puta

tion:

".

Page 24: A Users’ Manual and Tutorial for Performing COMET Structural

23

•T

he p

rope

rtie

s of

the

high

light

ed m

ater

ial c

an b

e vi

ewed

or

mod

ifie

d. C

lick

on "

Mat

eria

ls P

rope

rtie

s ...

" to

ope

n a

new

win

dow

(Fi

g. 9

(k)

) id

entif

ied

by th

e na

me

of th

e se

lect

ed m

ater

ial.

All

data

in th

is s

crol

labl

e w

indo

w, i

nclu

ding

the

mat

eria

l nam

e,

can

be m

odif

ied.

•T

o m

odif

y, d

oubl

e-cl

ick

or d

rag

with

mou

se b

utto

n pr

esse

d on

the

text

are

a. T

ype

over

the

high

light

ed a

rea

to r

epla

ce te

xt.

Clic

k on

"OK

" bu

tton

or e

nter

a c

arri

age

retu

rn to

acc

ept d

ata

chan

ge o

r "C

ance

l" b

utto

n to

neg

ate

the

chan

ge.

Clic

king

on

the

"App

ly"

butto

n

save

s th

e ch

ange

s an

d ex

its a

nd c

licki

ng o

n th

e "C

ance

l" b

utto

n qu

its w

ithou

t sav

ing

the

mod

ific

atio

ns.

Clic

k on

the

"A

pply

" bu

tton

.

Aft

er c

ompl

etin

g th

e m

ater

ials

spe

cifi

catio

ns,

clic

k on

the

"D

one"

but

ton

to r

etur

n to

the

mai

n m

enu.

Page 25: A Users’ Manual and Tutorial for Performing COMET Structural

24

Fig

ure

9 (a

)

Page 26: A Users’ Manual and Tutorial for Performing COMET Structural

25

Fig

ure

9 (b

)

Page 27: A Users’ Manual and Tutorial for Performing COMET Structural

26

Fig

ure

9(c)

F

igur

e 9(

d)

Page 28: A Users’ Manual and Tutorial for Performing COMET Structural

27

Fig

ure

9 (e

)

Page 29: A Users’ Manual and Tutorial for Performing COMET Structural

28

F

igur

e 9(

f)

Fig

ure

9(g

)

Page 30: A Users’ Manual and Tutorial for Performing COMET Structural

29

Fig

ure

9(h)

Fig

ure

9(i)

Page 31: A Users’ Manual and Tutorial for Performing COMET Structural

30

Fig

ure

9(j)

F

igur

e 9(

k)

Page 32: A Users’ Manual and Tutorial for Performing COMET Structural

31

Ass

igni

ng M

ater

ial a

nd S

ectio

n Pr

oper

ties

to th

e Fi

nite

Ele

men

ts

Hav

ing

sele

cted

the

mat

eria

ls w

hich

will

be

used

in f

orm

ulat

ing

the

fini

te e

lem

ent m

odel

, the

se m

ater

ials

and

sec

tion

prop

ertie

s

mus

t be

assi

gned

to th

e pr

evio

usly

def

ined

ele

men

t typ

es.

In th

is e

xam

ple,

all

EX

43 e

lem

ents

will

be

assi

gned

the

sam

e m

ater

ial (

Al

6061

-T6)

and

sec

tion

prop

ertie

s (0

.1"

thic

k).

The

abi

lity

to g

roup

ele

men

ts (

i.e.;

spar

s, r

ibs,

win

g sk

ins,

fus

elag

e fr

ames

, fus

elag

e sk

ins,

floo

rs, b

ulkh

eads

, etc

.) w

ill b

e in

clud

ed in

a la

ter

vers

ion

of A

CE

. T

he s

ectio

n pr

oper

ty id

entif

iers

whi

ch m

ust h

ave

data

def

ined

in th

is

step

are

ass

ocia

ted

with

the

elem

ent "

pid'

s" f

ound

in th

e PA

TR

AN

neu

tral

file

. Fo

r th

e m

ost s

impl

e m

odel

with

onl

y a

sing

le s

ectio

n

prop

erty

, onl

y on

e pr

oper

ty id

entif

ier

mus

t be

defi

ned.

The

"H

elp"

win

dow

(Fi

g. 1

0 (a

)) in

form

s th

e us

er o

f th

e nu

mbe

r of

sec

tion

type

s th

at h

ave

been

iden

tifie

d (o

ne f

or "

dem

o1"

and

two

for

"dem

o2")

and

dir

ects

the

user

to c

lick

on "

Sect

ion

Prop

s" in

the

cont

rol a

rea.

Clic

k on

the

"ra

dio"

but

ton

next

to

"Sec

tion

Pro

ps"

(gl

ows

red)

. Se

lect

ing

the

"Sec

tion

Prop

s" "

radi

o" b

utto

n di

spla

ys a

"SE

CT

ION

PR

OPE

RT

IES"

win

dow

alo

ng w

ith

an u

pdat

ed "

Hel

p" w

indo

w (

Fig.

10

(b))

. T

he "

SEC

TIO

N P

RO

PER

TIE

S" w

indo

w h

as,

•an

abb

revi

ated

for

m o

f th

e "H

elp"

inst

ruct

ions

;

•tw

o sc

rolle

d lis

t win

dow

s, o

ne to

hol

d th

e lis

t of

sect

ion

prop

erty

ids,

the

othe

r to

hol

d a

list o

f m

ater

ials

sel

ecte

d fo

r co

mpu

tatio

n;

•an

opt

ion

men

u to

def

ine

the

sect

ion

type

(H

omog

eneo

us, L

amin

ate,

Bea

m, C

ontin

uum

); a

nd

•tw

o pu

sh b

utto

ns c

alle

d "S

ectio

n Pr

oper

ties.

.." a

nd "

Don

e", o

ne f

or a

ssig

ning

mat

eria

l and

sec

tion

prop

ertie

s to

the

elem

ents

and

the

othe

r to

exi

t.

Page 33: A Users’ Manual and Tutorial for Performing COMET Structural

32

Fig

ure

10(a

)

Page 34: A Users’ Manual and Tutorial for Performing COMET Structural

33

Fig

ure

10(b

)

Page 35: A Users’ Manual and Tutorial for Performing COMET Structural

34

Fig

ure

10(c

)

F

igur

e 10

(d)

Page 36: A Users’ Manual and Tutorial for Performing COMET Structural

35

Fig

ure

10(e

)

F

igur

e 10

(f)

Page 37: A Users’ Manual and Tutorial for Performing COMET Structural

36

Follo

win

g th

e di

rect

ions

giv

en in

the

"Hel

p" w

indo

w,

•se

lect

a S

ectio

n ID

for

def

initi

on, p

lace

the

cur

sor

on t

op o

f a

Sect

ion

ID f

rom

the

Sec

tion

Pro

pert

y Id

. Lis

t an

dcl

ick

(Fig

. 10

(c))

whi

ch g

ives

the

follo

win

g re

sults

:

•th

e se

lect

ed S

ectio

n ID

is h

ighl

ight

ed,

•th

e as

soci

ated

ele

men

t typ

e is

iden

tifie

d by

the

labe

l

T

he E

lem

ent T

ype

Is :

(9 N

ode

Qua

drila

tera

l in

this

exa

mpl

e),

T

he T

ype

of S

ectio

n Is

: "o

ptio

n" m

enu'

s de

faul

t val

ue is

set

to th

e de

faul

t typ

e fo

r th

at e

lem

ent t

ype

( Hom

ogen

eous

in th

is

exam

ple)

and

•th

e us

er is

inst

ruct

ed to

sel

ect a

mat

eria

l fro

m th

e "D

efin

ed M

ater

ials

Lis

t:" a

s in

dica

ted

by F

igur

es 1

0 (

c) a

nd (

d).

Aft

er h

ighl

ight

ing

the

mat

eria

l sel

ectio

n (F

ig. 1

0 (e

)), a

new

"H

elp"

win

dow

(Fi

g. 1

0 (f

)) a

dvis

es th

e us

er a

bout

the

sect

ion

type

s

avai

labl

e an

d th

en in

stru

cts

him

/her

to c

lick

on t

he "

Sect

ion

Pro

pert

ies

..."

butt

on.

A d

ata

inpu

t win

dow

(Fi

g. 1

0 (g

)) ti

tled

with

the

sele

cted

sec

tion

type

("H

omog

eneo

us",

in th

is e

xam

ple)

is n

ow o

pene

d an

d th

e

sec

tion

and

the

mat

eria

l ide

ntif

icat

ion

num

bers

are

fill

ed in

the

corr

espo

ndin

g fi

elds

as

desc

ribe

d in

the

"Hel

p" w

indo

w (

Fig.

10

(h))

The

"Hel

p" w

indo

w a

lso

lists

the

rem

aini

ng in

put r

equi

rem

ents

for

the

sect

ion

prop

ertie

s of

this

par

ticul

ar e

lem

ent t

ype

.

Inst

ruct

ions

for

ent

erin

g or

mod

ifyi

ng d

ata

in th

ese

inpu

t win

dow

s w

as d

iscu

ssed

ear

lier

whe

n de

scri

bing

mat

eria

l pro

pert

ies.

Aft

er c

ompl

etin

g th

e da

ta in

put (

a th

ickn

ess

of 0

.1 in

. was

use

d fo

r th

is e

xam

ple)

, clic

k on

the

"A

pply

" bu

tton

. T

he u

ser

now

rev

erts

to th

e "S

EC

TIO

N P

RO

PER

TIE

S" w

indo

w a

nd s

elec

ts a

noth

er s

ectio

n pr

oper

ty I

D u

ntil

the

list i

s ex

haus

ted.

Page 38: A Users’ Manual and Tutorial for Performing COMET Structural

37

Fig

ure

10(g

)

F

igur

e 10

(h)

For

the

"dem

o2"

PAT

RA

N m

odel

file

, the

sec

ond

sect

ion

ID r

epre

sent

s a

Bar

/Bea

m, a

s in

dica

ted

by th

e ye

llow

text

, (Fi

g.. 1

0 (i

))

and

" The

Typ

e of

Sec

tion

is: "

has

bee

n se

t to

"Bea

m".

Jus

t lik

e be

fore

, sel

ecti

ng t

he m

ater

ial a

nd th

en c

licki

ng o

n "S

ecti

onP

rope

rtie

s ...

" bu

tton

will

ope

n th

e da

ta in

put w

indo

w (

Fig.

10

(j))

that

is ti

tled

"Bea

m"

and

•di

spla

ys th

e id

entif

icat

ion

num

bers

of

the

sect

ion

and

the

mat

eria

l pro

pert

ies

as p

revi

ousl

y se

lect

ed (

Fig.

10

(k))

and

•id

entif

ies

the

inpu

t req

uire

men

ts r

equi

red

to d

escr

ibe

the

sect

ion

prop

ertie

s fo

r th

is p

artic

ular

ele

men

t typ

e.

Page 39: A Users’ Manual and Tutorial for Performing COMET Structural

38

Fig

ure

10(i

)

In th

e ne

xt r

elea

se o

f A

CE

, an

inte

ract

ive

grap

hics

win

dow

will

dis

play

the

beam

cro

ss-s

ectio

n, it

s di

men

sion

s an

d or

ient

atio

n.

Alth

ough

, PA

TR

AN

req

uire

s th

at th

e or

ient

atio

n al

l 1-d

imen

sion

al e

lem

ents

(i.e

.; be

ams)

be

spec

ifie

d at

the

time

of th

eir

gene

ratio

n, th

ene

xt r

elea

se w

ill s

how

this

ori

enta

tion

and

perm

it it'

s m

odif

icat

ion.

Fo

r th

e pr

esen

t tim

e, it

is s

ugge

sted

that

Iy-

y an

d I z

-z r

epre

sent

the

max

imum

and

min

imum

pri

ncip

al m

omen

ts o

f in

ertia

, res

pect

ivel

y, a

nd th

at th

e to

rsio

nal r

igid

ity r

epre

sent

s th

e po

lar

mom

ent o

f in

ertia

,

all m

omen

ts o

f in

ertia

with

res

pect

to th

e ce

ntro

id.

Als

o, th

e ab

ility

of

a be

am to

sup

port

tors

ion

is s

omew

hat c

ompl

ex f

or n

on-c

ircu

lar

sect

ions

and

this

com

plex

ity w

ill a

lso

be d

ealt

with

in a

late

r ve

rsio

n. A

ctua

lly, t

his

late

r ve

rsio

n w

ill a

ccom

mod

ate

the

grou

ping

of

one-

Page 40: A Users’ Manual and Tutorial for Performing COMET Structural

39

dim

ensi

onal

ele

men

ts s

uch

that

they

can

be

desc

ribe

d as

axi

al r

ods,

tors

ion

bars

, she

ar/m

omen

t bea

ms,

or

full

load

car

ryin

g (a

xial

, she

ar,

tors

ion,

and

ben

ding

) be

ams

as w

as m

entio

ned

earl

ier

for

sele

ctin

g va

riou

s pl

ate

and/

or s

hell

elem

ents

(i.e

.; sh

ear

and

mem

bran

e/be

ndin

g

elem

ents

whi

ch w

ould

be

used

to m

odel

a w

ing)

that

may

be

need

ed to

def

ine

a st

ruct

ure.

Fig

ure

10(j

)

F

igur

e 10

(k)

Page 41: A Users’ Manual and Tutorial for Performing COMET Structural

40

Fig

ure

10 (

l)

Fig

ure

10 (

m)

Hav

ing

spec

ifie

d th

e se

ctio

n pr

oper

ties

for

the

beam

ele

men

t, cl

ick

on t

he "

App

ly"

butt

on.

The

use

r is

now

ret

urne

d to

the

"SE

CT

ION

PR

OPE

RT

IES"

win

dow

(Fi

g. 1

0 (l

)) a

nd a

new

"H

elp"

win

dow

(Fi

g. 1

0 (m

)) in

form

s th

e us

er th

at if

all

sect

ion

prop

erty

dat

a

has

been

def

ined

for

all

the

Sect

ion

IDs,

clic

k on

"D

one.

Page 42: A Users’ Manual and Tutorial for Performing COMET Structural

41

Spec

ific

atio

n of

Sol

utio

n C

onst

rain

ts

The

initi

al s

ize

of th

e st

iffn

ess

mat

rix

is d

eter

min

ed b

y as

sign

ing

a fu

ll si

x de

gree

s of

fre

edom

to e

ach

node

of

the

fini

te e

lem

ent

mod

el.

For

thos

e m

odel

s in

whi

ch th

e el

emen

ts c

onne

cted

to th

e no

des

do n

ot r

epre

sent

a s

tiffn

ess

com

pone

nt in

one

or

mor

e of

the

degr

ees

of f

reed

om, t

hen

thes

e pa

rtic

ular

deg

rees

of

free

dom

sho

uld

be d

elet

ed f

rom

the

mod

el a

nd th

e st

iffn

ess

mat

rix

will

be

redu

ced

acco

rdin

gly.

For

exa

mpl

e, a

fla

t pan

el s

ubje

cted

to a

n in

-pla

ne te

nsile

or

com

pres

sive

load

cou

ld b

e m

odel

ed w

ith m

embr

ane

or

mem

bran

e/be

ndin

g pl

ate

elem

ents

, and

the

degr

ees

of f

reed

om r

epre

sent

ing

the

out-

of-p

lane

tran

slat

ion

and

rota

tion

(oft

en c

alle

d th

e

drill

ing

degr

ee o

f fr

eedo

m)

abou

t all

thre

e ax

es w

ould

be

elim

inat

ed.

In s

ome

CO

ME

T a

pplic

atio

ns, t

here

is a

n au

tom

atic

sup

pres

sion

of

the

drill

ing

degr

ees

of f

reed

om a

nd m

ore

cons

ider

atio

n w

ill b

e gi

ven

to th

is in

late

r A

CE

ver

sion

s su

ch th

at th

e us

er w

ill b

e ad

vise

d of

such

and

off

ered

pos

sibl

e fi

xes.

Aft

er th

e us

er h

as d

efin

ed th

e m

ater

ial a

nd c

ross

-sec

tiona

l pro

pert

ies

of th

e va

riou

s el

emen

t typ

es, t

he s

cree

n is

ref

resh

ed (

Fig.

11

(a))

with

a n

ew "

Hel

p" w

indo

w th

at a

dvis

es th

e us

er o

f w

heth

er o

r no

t any

con

stra

ints

des

crib

ing

the

boun

dary

con

ditio

ns h

ave

been

spec

ifie

d. T

he s

peci

fica

tion

of c

onst

rain

ts th

at r

epre

sent

the

boun

dary

con

ditio

ns o

f th

e st

ruct

ure

(i.e

.; si

mpl

y su

ppor

ted

or f

ixed

edg

es)

can

be a

ccom

plis

hed

at th

is ti

me

or th

e co

nstr

aint

s de

fine

d in

the

impo

rted

mod

el f

ile c

an b

e m

odif

ied.

For

the

dem

onst

ratio

n pr

oble

ms

("de

mo1

" an

d "d

emo2

"), t

he b

ound

ary

cond

ition

s w

ere

defi

ned

in th

e PA

TR

AN

mod

el a

nd im

port

ed v

ia th

e ne

utra

l file

.

Due

to th

e pr

edet

erm

ined

seq

uenc

ing

of a

ctio

ns in

the

"QU

ER

Y"

mod

e, th

e us

er is

requ

ired

to

clic

k on

the

"ra

dio"

but

ton

adja

cent

to

"BC

" (s

ee "

Hel

p" w

indo

w).

The

use

r m

ay r

evie

w th

e de

fine

d bo

unda

ry c

onst

rain

ts (

here

, the

y re

pres

ent f

ixed

rot

atio

nal

cons

trai

nts

alon

g th

e ed

ges

and

tran

slat

ion

only

in th

e x-

dire

ctio

n) b

y cl

icki

ng o

n th

e "C

onst

rain

t" b

utto

n in

the

"D

efin

eC

onst

rain

ts"

win

dow

(see

Fig

. 11

(b)

and

corr

espo

ndin

g "H

elp"

win

dow

). T

his

will

ope

n th

e "A

pplie

d D

ispl

acem

ent D

ialo

g"

win

dow

sho

wn

in F

igur

e 11

(c).

Page 43: A Users’ Manual and Tutorial for Performing COMET Structural

42

Fig

ure

11 (

a)

Page 44: A Users’ Manual and Tutorial for Performing COMET Structural

43

For

the

dem

onst

ratio

n pr

oble

m c

hose

n to

illu

stra

te th

is g

raph

ical

use

r in

terf

ace

("de

mo-

2"),

the

edge

s w

ere

inte

nded

to b

e to

tally

cons

trai

ned

in th

e ou

t-of

-pla

ne (

z) tr

ansl

atio

n an

d th

e ro

tatio

ns a

bout

the

x an

d y

axes

. Scr

ollin

g do

wn

the

list o

f co

nstr

aine

d no

des

and

sele

ctin

g ea

ch n

ode,

one

at a

tim

e, b

y pl

acin

g th

e cu

rsor

on

the

node

num

ber

and

clic

king

, the

sel

ecte

d no

de is

sho

wn

dire

ctly

belo

w th

e lis

t of

node

s an

d its

app

lied

cons

trai

nts

are

show

n be

low

the

sele

cted

nod

e. T

he "

radi

o" b

utto

n fo

r th

e co

nstr

aine

d no

de is

turn

ed o

n (r

ed g

low

) an

d th

e en

forc

ed d

ispl

acem

ent o

r ro

tatio

n is

sho

wn

to th

e ri

ght.

The

se c

onst

rain

ts c

an b

e se

t fix

ed o

r fr

ee b

y cl

icki

ng

on th

e "r

adio

" bu

tton

and

the

enfo

rced

dis

plac

emen

t val

ue c

an b

e sp

ecif

ied

as p

revi

ousl

y de

scri

bed

for

data

inpu

t dia

logs

. R

evie

win

g th

e

list o

f co

nstr

aint

s w

ill r

evea

l tha

t the

edg

e (n

odes

25

and

27 th

roug

h 30

as

show

n in

Fig

ure

11 (

c)),

whe

re th

e in

-pla

ne te

nsile

load

will

be

appl

ied,

has

not

bee

n co

nstr

aine

d. T

o re

stri

ct d

ispl

acem

ents

alo

ng th

is e

dge

to e

long

atio

n al

ong

the

x-ax

is, w

e w

ill a

pply

con

stra

ints

to

the

inte

rior

nod

es (

node

s 27

thro

ugh

29)

as f

ollo

ws:

•In

the

botto

m d

ata

win

dow

title

d, "

Con

stra

in N

ode

Num

ber

(and

<C

R>

):"

of th

e "A

pplie

d D

ispl

acem

ent D

ialo

g" w

indo

w (

Fig.

11

(d))

, ent

er 2

7 (s

ee "

Hel

p" w

indo

w a

s ill

ustr

ated

in F

igur

e 11

(e)

).

•R

evie

w th

e co

nstr

aint

set

ting

(Fig

. 11

(f))

and

clic

k on

"ra

dio"

but

ton

adja

cent

to

"W",

x", a

nd "

Θy"

(re

d gl

ow o

f

the

"rad

io"

butto

n m

eans

that

par

ticul

ar d

egre

e of

fre

edom

at n

ode

27 is

con

stra

ined

).

If c

onst

rain

ts a

re in

dica

ted

for

othe

r de

gree

s of

free

dom

(i.e

.; "U

", "

V"

and/

or "

Θz"

), c

lick

on th

e "r

adio

" bu

tton

adja

cent

to th

at d

egre

e of

fre

edom

(a

gray

but

ton

mea

ns

unco

nstr

aine

d).

• C

lick

on t

he "

Add

" bu

tton

to in

corp

orat

e th

e ne

w c

onst

rain

ed n

ode

to th

e m

odel

. In

this

exa

mpl

e, th

e en

forc

ed d

ispl

acem

ent

at a

ll no

des

has

been

unc

hang

ed f

rom

the

defa

ult v

alue

of

0.0.

•R

epea

t th

e ab

ove

thre

e st

eps

for

node

s 28

and

29

and

then

clic

k on

the

"D

one"

win

dow

.

•T

o de

lete

a c

onst

rain

ed n

ode

from

the

list,

sele

ct th

e no

de a

nd u

ncon

stra

in a

ll de

gree

s of

fre

edom

by

clic

king

on

the

red

"rad

io"

butto

ns a

ssoc

iate

d w

ith th

e no

de.

Page 45: A Users’ Manual and Tutorial for Performing COMET Structural

44

Fig

ure

11 (

b)

Page 46: A Users’ Manual and Tutorial for Performing COMET Structural

45

Fig

ure

11 (

c)

Page 47: A Users’ Manual and Tutorial for Performing COMET Structural

46

Fig

ure

11 (

d)

Fig

ure

11 (

e)

Page 48: A Users’ Manual and Tutorial for Performing COMET Structural

47

Fig

ure

11 (

f)

Page 49: A Users’ Manual and Tutorial for Performing COMET Structural

48

Spec

ific

atio

n of

App

lied

Loa

ds

As

illus

trat

ed in

Fig

ure

12 (

a), t

he u

ser

is n

ow r

etur

ned

to th

e co

ntro

l are

a an

d th

e "H

elp"

win

dow

info

rms

him

/her

abo

ut th

e

exis

tenc

e or

non

-exi

sten

ce o

f pr

evio

us lo

ad c

ase(

s) d

efin

ed in

PA

TR

AN

.

The

use

r is

now

req

uest

ed to

clic

k on

the

"ra

dio"

but

ton

adja

cent

to

"Loa

ds"

whi

ch o

pens

the

"Def

ine

Loa

ds"

win

dow

as s

how

n in

Fig

ure

12 (

b).

The

pro

cedu

re f

or a

ddin

g ne

w lo

adin

g co

nditi

ons

or m

odif

ying

exi

stin

g lo

adin

g co

nditi

ons

is id

entic

al to

the

proc

edur

e de

scri

bed

for

boun

dary

con

ditio

ns.

The

"D

efin

e L

oads

" w

indo

w in

clud

es a

n "O

ptio

n" m

enu

whi

ch a

llow

s fo

r th

e se

lect

ion

of v

ario

us ty

pe o

f lo

ads.

As

with

all

"Opt

ion"

men

us, p

lace

the

cur

sor

on t

op o

f th

e "O

ptio

n" b

utto

n an

d de

pres

s th

e m

ouse

but

ton

to d

ispl

ay th

e va

riou

s

type

s of

load

s th

at c

an b

e ad

ded

or m

odif

ied.

Whi

le d

epre

ssin

g th

e m

ouse

but

ton,

dra

g th

e cu

rsor

to th

e de

sire

d lo

ad ty

pe.

Onl

y th

e

"For

ce"

optio

n ca

n be

sel

ecte

d fo

r th

is in

itial

ver

sion

and

thos

e sh

own

in g

ray

are

plan

ned

for

late

r ve

rsio

ns.

Als

o, th

is in

itial

ver

sion

can

only

acc

omm

odat

e a

sing

le lo

ad c

ase

but l

ater

ver

sion

s w

ill h

andl

e se

vera

l loa

d ca

ses

and

com

bina

tions

of

vari

ous

load

cas

es.

Sinc

e a

desc

ript

ion

of th

is in

put w

indo

w is

nea

rly

iden

tical

to th

e "A

pplie

d D

ispl

acem

ent D

ialo

g" w

indo

w, c

lick

on t

he"C

ance

l" b

utto

n to

mov

e on

to th

e ne

xt it

em in

the

cont

rol a

rea.

Thi

s co

mpl

etes

the

phys

ical

des

crip

tion

of th

e fi

nite

ele

men

t mod

el.

Not

e : T

he d

ispl

ay o

f th

e ap

plie

d fo

rces

pre

sent

in th

e in

itial

mod

el is

pos

sibl

e th

roug

h in

tera

ctio

n w

ith C

Gx,

the

CO

ME

T G

raph

ic

proc

esso

r.

Page 50: A Users’ Manual and Tutorial for Performing COMET Structural

49

Fig

ure

12 (

a)

Page 51: A Users’ Manual and Tutorial for Performing COMET Structural

50

Fig

ure

12 (

b)

Page 52: A Users’ Manual and Tutorial for Performing COMET Structural

51

Spec

ific

atio

n of

the

Res

ults

A

fter

bei

ng r

etur

ned

to th

e co

ntro

l are

a (F

ig. 1

3 (a

)), t

he u

ser

is r

eque

sted

to c

lick

on "

Pre

fere

nces

" on

the

men

u ba

r an

d

sele

ct "

Ana

lysi

s ...

" fr

om th

e pu

ll do

wn

men

u (F

ig. 1

3 (b

)).

"Pre

fere

nces

" al

low

s th

e us

er to

sel

ect t

he ty

pe a

nd f

orm

at o

f th

e re

sults

and

the

met

hod

for

disp

layi

ng a

nd/o

r re

port

ing

sam

e. O

nly

the

"Ana

lysi

s" o

ptio

n is

ope

ratio

nal i

n th

is in

itial

ver

sion

.

Fig

ure

13 (

a)

Fig

ure

13 (

b)

Page 53: A Users’ Manual and Tutorial for Performing COMET Structural

52

Sele

ctin

g th

e "A

naly

sis

..."

optio

n op

ens

the

"LIN

EA

R S

TA

TIC

AN

AL

YSI

S" w

indo

w a

nd c

orre

spon

ding

"H

elp"

win

dow

sho

wn

in F

ig. 1

3 (c

). T

he "

LIN

EA

R S

TA

TIC

AN

AL

YSI

S" w

indo

w m

akes

dir

ect q

ueri

es o

f th

e us

er w

hich

can

be

answ

ered

with

a "

Yes

" or

"No"

. T

he c

hose

n re

spon

se w

ill b

e hi

ghlig

hted

with

a r

ed g

low

.

Ans

wer

ing

"Yes

" to

que

stio

n 1

will

cau

se a

dditi

onal

que

ries

to b

e di

spla

yed

as s

how

n in

Fig

. 13

(d).

The

se q

uest

ions

rel

ate

to th

e

coor

dina

te s

yste

m o

f th

e co

mpu

ted

stre

sses

(i.e

.; el

emen

t or

glob

al a

xes

syst

em)

and

thei

r lo

catio

n (i

.e.;

node

s, c

entr

oids

, or

inte

grat

ion

poin

ts).

Fut

ure

vers

ions

will

allo

w f

or th

e se

lect

ions

of

stre

sses

that

cor

resp

ond

to v

ario

us f

ailu

re th

eori

es (

e.g.

., vo

n M

ises

, max

imum

shea

r st

ress

, etc

. for

the

isot

ropi

c m

ater

ials

and

Tsa

i-W

u, H

offm

an, e

tc. f

or th

e or

thot

ropi

c m

ater

ials

).

Onc

e th

e ty

pe a

nd f

orm

at o

f th

e re

ques

ted

outp

ut is

spe

cifi

ed, c

lick

on t

he "

AC

CE

PT

" bu

tton

. T

his

com

plet

es th

e

deve

lopm

ent o

f a

CO

ME

T r

unst

ream

.

Not

e: P

laci

ng th

e cu

rsor

and

clic

king

on

the

ques

tions

will

pro

vide

hel

p on

that

que

stio

n in

the

"Hel

p" w

indo

w.

Page 54: A Users’ Manual and Tutorial for Performing COMET Structural

53

Fig

ure

13 (

c)

Page 55: A Users’ Manual and Tutorial for Performing COMET Structural

54

Fig

ure

13 (

d)

Exe

cutio

n

Now

that

the

runs

trea

m h

as b

een

deve

lope

d an

d ac

cept

ed, t

he u

ser

is r

etur

ned

to th

e co

ntro

l are

a an

d as

ked

to c

lick

on t

he"E

xecu

tion

" bu

tton

(Fi

g. 1

4 (a

)).

The

"M

odel

Exe

cutio

n D

ialo

g" w

indo

w is

now

ope

ned,

as

show

n in

Fig

ure

14 (

b), a

nd th

e us

er is

requ

este

d to

rev

iew

his

/her

run

stre

am s

peci

fica

tions

and

then

clic

k on

the

larg

e "E

xecu

tion

" bu

tton

. T

he u

ser

is a

dvis

ed (

Figu

re

14 (

c))

that

the

CO

ME

T r

unst

ream

is b

eing

ass

embl

ed a

nd im

med

iate

exe

cutio

n w

ill f

ollo

w.

The

run

stre

am f

ile is

cre

ated

in th

e w

orki

ng

dire

ctor

y w

ith th

e fi

lena

me

base

d on

the

mod

el in

put f

ile n

ame

and

the

anal

ysis

type

with

the

exte

nsio

n ".

com

" ap

pend

ed.

It is

exe

cute

d

as a

bac

kgro

und

job,

and

aft

er e

xecu

tion

is c

ompl

ete,

the

user

is r

etur

ned

to th

e A

CE

con

trol

are

a.

The

log

file

fro

m t

he a

naly

sis

exec

utio

n is

in th

e cu

rren

t dir

ecto

ry w

ith th

e sa

me

root

file

nam

e as

the

runs

trea

m a

nd th

e ex

tens

ion

of "

.log"

. B

oth

the

run

stre

am f

ile

and

the

log

file

are

text

file

s w

hich

may

be

view

ed, e

dite

d, a

nd p

rint

ed o

utsi

de o

f A

CE

, if

desi

red.

Page 56: A Users’ Manual and Tutorial for Performing COMET Structural

55

Fig

ure

14 (

a)

Page 57: A Users’ Manual and Tutorial for Performing COMET Structural

56

Fig

ure

14 (

b)

Page 58: A Users’ Manual and Tutorial for Performing COMET Structural

57

Fig

ure

14 (

c)

Eva

luat

ing

and

Rep

ortin

g th

e R

esul

ts

Pres

ently

, the

"R

esul

ts"

part

of

AC

E h

as n

ot b

een

impl

emen

ted.

How

ever

, gra

phic

al v

iew

s of

the

resu

lts c

an b

e ob

tain

ed v

ia C

Gx

whi

ch h

as b

een

inte

rfac

ed w

ith th

e C

OM

ET

res

ults

dat

abas

e. A

s pr

evio

usly

sta

ted,

dir

ectio

ns f

or u

sing

CG

x ar

e no

t int

ende

d to

be

part

of

this

use

rs' m

anua

l. H

owev

er, l

ater

ver

sion

s of

AC

E w

ill in

clud

e a

self

-con

tain

ed c

apab

ility

for

gen

erat

ing

vari

ous

grap

hica

l pre

sent

atio

ns

of d

ata

(i.e

.; co

ntou

rs, x

-y, d

efor

med

and

und

efor

med

, etc

.) a

nd r

epor

t for

ms

(i.e

.; ta

bles

).

For

the

incl

uded

dem

onst

ratio

n pr

oble

m (

"dem

o2")

, a C

Gx

gen

erat

ed c

onto

ur p

lot o

f th

e no

rmal

str

esse

s in

the

x-di

rect

ion

is

show

n in

Fig

ure

15.

All

the

resu

lts r

eque

sted

in "

Pref

eren

ces"

are

giv

en in

the

outp

ut f

ile c

alle

d "d

emo2

_lst

atic

.log"

. In

gen

eral

, the

nam

e of

this

file

iden

tifie

s th

e na

me

of th

e m

odel

("d

emo2

") a

nd th

e ty

pe o

f an

alys

is (

linea

r st

atic

). S

ince

this

file

is a

log

of th

e ex

ecut

ion

of th

e A

CE

gen

erat

ed C

OM

ET

run

stre

am, i

t cou

ld b

e re

view

ed in

cas

e of

pos

sibl

e ex

ecut

ion

erro

rs (

Hea

ven

Forb

id!!

!).

Perf

orm

ing

Ano

ther

Ana

lysi

s or

Qui

tting

As

indi

cate

d in

the

"Hel

p" w

indo

w o

f Fi

gure

(15

), a

new

ana

lysi

s ca

n be

gin

by s

elec

ting

a m

odel

file

fro

m th

e "F

ile"

pull

dow

n

men

u or

the

inte

rfac

e ca

n be

exi

ted

by c

licki

ng o

n "Q

uit"

in t

he c

ontr

ol a

rea.

Ano

ther

"po

p-up

" w

indo

w (

Fig.

16)

will

app

ear

in

the

uppe

r ri

ght h

and

corn

er a

nd g

ives

the

user

ano

ther

cha

nce

to d

ecid

e. L

et u

s qu

it w

riti

ng a

nd d

emon

stra

ting

by

clic

king

aso

lid "

Yes

"!!!

!

Page 59: A Users’ Manual and Tutorial for Performing COMET Structural

58

Fig

ure

15

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