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On certain approximations in the finite-element method

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-5

1975

ARCH1EF

Nomenclature

= value of approximate

solu-tionatz =

g, G = exact, approximate

fwsc-fions (g = ce) nìiiiínitni value of g

1, ja = functionals of variational

principles M1, M2, Jf = positive numbers 58

/ MARCH 1971

liitrou cl io n

IN the aipIualioit of tise flnite-elenwnt method [1,

2] Ito cuniplex problems il i.s often Ilsefill to make zspproxintatiolss that are outside of the I Iit'ory of varialional calculus, For

ex-ample, iii many dynamic tiialyses il. is useful to lump themass of

the system by some rule of experience. The 1(51 ut is a diagonal mass matrix that is easier tu handle thaii a colisisteuil mass matrix 13] which is coupled. iniilarly, tise stillness matrix for als

ele-ment is generally derived with certain simplifying assumptions.

The cross-sectional area, moment of inertia, material, etc., usually are assumed to be constants over ais element. These

approxima-Numbers in brackets de,.ig,iatc Ileferences at end ofpaper.

Contributed by the Applied i\Ic,lsnnks Division and presented at

the Winter Annual Meeting, New York, N. Y., November 29-December 3, 1970, of THE AMERICAN SOCIETY OF MECHANICAL

ENGINEERS.

Discussion of this paper should be addressed to the Editorial De-partment, ASME, Tnjte Engineering ('enter, 345 East 47th Street, New York, N. Y. 101)17, and will he accepted until April 20, 1971.

Disusiun received after the closirlg date will be returned. Manu-script received by ASME Applied Mechanics Division, October 20,

lt-liti; final revision, January 30, 1970 Paper No. 70-WA/APM-34.

On Certain Approximations in the

Finite-Elemeiit Method

Approximations made outsideof the variational principle used in the finite-element

iiiet hod are examined for a restricted problem in elasticity. They are s/town to be riorous

front the standpointofa generalized variational principle in which Lagrange multipliers are utilized. The convergence oflite Ritz solution to 1h e exact solution is demonstrated. The bound is shown to he a functionofthe qualityofboth the displacement functions and oilier approximate f unclions in tite a nalysis.

Lab.

y.

Scheepsbouwkunde

Technische Hogeschool

Deift

= extremal function of I

(exact solution)

ii0 = extremal function of I i5f

= first variations of

fune-tionals

Xg À = Lagrange multiplier

func-tions

Transactions o the ASME

at ('

ssu

di

X

X r O. XrL

Fig. i(a) Boundary-value problem

110115 are desirable 5juni I mvmeducc tite complexity of derivations luid simplify coding and (lcbugging of the digital programs. From

experience we know that they IISU:llly du not affect the quality of

the approximate solution. However, there still remain several questions. Why do we obtaiui a good approximate solutiotI to it

coulIplex problem when we usiake approximations outside nf the theory of variational calculus? how do we obtain the sollutioml? What are tise error relatioisships betweefl the approximate solis-lions and the exact solution to the problem? This work attempts

to partially answer these questions by examining a restricted

problem in the light of the approximation theory. An Investigation

We examine here the problem of tise rod loaded by a body force

q shown in Fig.

i(a), l'bis probleun is the simplest mixed

boundary-value problem in elasticity. We

assume that g =

ae > 0, the product of the area and elastic modulus, is a

piece-n = piece-number of elemepiece-nts ipiece-n

finite-element mesh

q, Q = exact, approximate

body-force fwsctions

U = approxi mate displacement

function

= Ritz function

R. W. MCLAY

Associate Professor, Department of Mechanical Engineering, University of Vermont,

(2)

X:O X Fig. 1(6) Example function g

X:O. )t=L

Fig. 1(c) Example function q

e diitreri i al >Je fi r ti ni ro id ib at q is a piecewise continuous

Irr. F;XilIii)i finiti iiiris for q, q are shown in Figs. i (b, e).

fl

t\ati soliti loi i to titeproblem posed in Fig. I will sal isfy i Li erer ii irtiequation

d

f

ii

\

-

(g

J

+

q = O

dx\

(LV,

at p ii Is at which (dg/iI.r),q are coin ri nous arai t he t ranisit ion

11115

=

itt

iris ¿ where either or both (dg/dx), q

arediscorithuions.

Tri zìdlitioii

lii irder to obtain roiripprcxi ni atesol uit ji ut tot his prinbleni lu'

using the flruite-elenieiit rnethuiil we make lise of the following f unit ronrui

11

'il

= 2j>

g Uix) dx

-

qUdx

.J(i

whiri. U isan apptoximritefunctionsatisfying theessential

eon-(ijtioiiï

I

UC()

wilinini ihs elements,

-, U

= at element boundaries, (5) 3

UrO

= O. If we choose U as

U =

a

+

(asi - a) (

J (6)

-Witiuiuia fInite element where a0 a+ are vali

lesof the approximate

solitI ioni at, the left arid right elenienitboundaries x0

respec-tively, it cari be shown[4-Ji] t hat the

flitz

solution obtained with (J arid the funìctionalof equation (4) coiiverge to the exact

soin-lion , on refinementof the finite-element mesh.

Let us

desig-nate the flitz soltition as U11. The sense of convergencet>f itSfollows:

fL(du

j)2

dx <

!',

JUR - uJ

(L2)h/2

(7)

Where n is the nuniiruirer ofcl>rireiiis in lite analysis and21f1,M2are

Journal of Applied Mechanics

(4)

positive ritniniliers. 1(luiit tue ?l>vel?l?lirenut if eciurrtjoni (7)is (nIy luruilrin' to tine work >f i efenrnii loi i t will riot, he prescrit ed here.

We i uext ileveli ilIi nie i iiI eint, rif this work, a t,u1(1g of

ap-poixi nrii inrisheytuiiil I lun ii illoweuli,v the essential corel t ionsof

t Ii> originalfinitiii tuai lu tii irtt.ioit (4). Suppose that itis

meurt-veu uienit to evntl ini le tine ini (grals ofequation (4) di IC lo i he

corn-l>leity of generati rig t lii fiiii ilions g, q. We crini sim Ill fy the

problem byapprox juunaiirg these functions. Titis eroi he ji isti fled

by the tise of Lagrriruge niuiil i pIers. l'ue funnuctiottal of equation (4) then becomes

i

1"

IdU\

¡'L

= -

2J0

I

G ( -

\dx/

I

(Ix -

I QUdx

J0

+

j

iXg(G - g) + À5(Q - q)Jdx, (S) where G,Qare fuiictionuii ripproxirurit inng g, q, respectively, arid XQ À5 aie Lagrange muli iplier functions imposi rig approximate

equality of the fiiiretiouu l)airs. Note that this approach brings

the approximation of the functions g, q within the variational principle. We can further extend nur discussion of equation (S)

h iimiting (lie variations of (lie approximate functions G, Qsuch that the third integral is zero. On doiuug this I becomes

1

fL

G

(?!)2

i/x

L

QUdx. (9)

-

dx

Itenauise l is not t lu?' annre J the extreunril funictiout u0 of I

will sat isfy a differeni t l in lcr(II? ial ii uni nu rial ural troriditionis

than

tliuir.i' 1 '1'}us linI,i >Iluutit >tiof l(; 15

nl /

diu1\

-- ( (i

- - J

+

(J =

Lr

nix,

'a-i t bui t lie elenueints Iul k, t he natural conudiiioiis are il,u G----"

=G---'

dx x= dx (1111

G--'1

dx

=0.

a

I'he theory of Lrigr:uuige nuuuil t pliers shows us that the

ripproxi-inritiouis in eqnialioru (S) (arid (9) ris well) are correct. Yet, if u9 and 0G satisfy ditfereiitt Euler equrrtiu)uas and natural conditions

t hey cannot he the same furìctiont. I luw then do we obtain a soiu-tioni to ihe original prohulinui?

The answer to this qnuist unni Iic irr the study of convergence of

tire solutions, which will mow be developed.

This study will

show that the flitz soluttinir Uz associated with Io approaches 0G while u0 approaches the exact solution u, both approaches being uniform.

Tire first derivatives itt each ease approach in the

ineaii.

Let us make the essential condii ions of J anni the suinte, =

uJ0 = o.

Then u0 is admissible to 'u riunii, sinarilruiiv, u is admissible to It;. Oir substitution anid by nirikiuig use of tire fact that älg= = O for ali admissible futtictions it is possible to show that

L fn/ui0 2

1(u) - 1(in) = f g

-

dx 0,

Ï0(u) - IG(ilG)

=

f G

(n/uu dx 0. 2 dx dx

MARCH 1971 / 59

X Xi (IO) dU g__i? dx X = - (2)

If we now further i'it riet ourselves to approximate functions

G > (I, we have a minimum ninuciple. It is interesting that the ftiincliouirul I; of equation I)) is ri nuinuimuimn principle aiuti yet is

i nrplied I y thefuinuctin >tutul 1,; tf equi at ioni (M) which

is riot it mi

ni-mii ni priru ripie. Ni ile :tIu u th uit le of equal inri (9)15 not tItesame

nnuiuuniiuinn principle as I, uf equal 'iii (4).

= O,

('iii?

= t). (3)

(3)

TItt' basic teqiinlit tes of eilt loti (13) are a st itt erneut of the

utili nomi pri itt-i pies, t lie i t it egut ts bei tig tite sou it id variations of

thet'e--.lie(-t ive fitmietionals.

We next add tltee

two inequalities

ttt obt titi

J9(u1) - ¡12(u0) -4- 1(ti,)

t0(u)

i

(due

(lU'\2 L (due

(/ti\2

= -

tii-

-

i

u'.r+

2

\ dx

dxj

2

\

dx dx L

¡j

/ì\2

g ii 0G I (IX > 0. 2

\dz

dxj

We expa t al arid rea rialigeCIII 1:1 t ion(14)to obtai ti

j

(g - (;)

(duo)

dx

jL

(q -

Q)u0dx 2

+

¡ 1L

(( - g)

(dy

/

1L

- q)udx

I Lg (du0 dx 0. (13)

2J0

\dx

(IX/

Next, we rearrange equation (15),

i

("

/du02

de 2\

rL

-

(gG)(

Jdx

(qQ)(u0--u)dx

2

\

dx

dx /

¡-'L 1d h

, ¡

f_2_Li()

dx0. (16)

2J0

\dx

dx,

We develop two basic inequalities by making tise of equations (3) and (3).

lue -

nul =

IftItiQ

I----

\dx

(Ix/

/u\

-Jdx

< L" [

çL

(duo

,/,,\2

dxl

-

L.J

\dx

il.r/

J

r

rLld1i0

du \2

J

XI

I

j____P)

dx

[J0 \dx

dx/

-

f1.

(q -

Q)(u0 - u0)dx

<[fL

1/2 L (q Q)2dx]

[f (u0 -

uQ)2dx]

-

o (17)

Also, the right-hat id ntot iii ter of eq u a t lt t t (16)

can be bouinidej

below with the knowledge that.g miu> (i. Thins

i

('

(du0

du\2

gv--- I

(IX 2

\dx

dx/

I / J ( (/(1t(/ (.0 0. (21)

2J

\dx

dx/

On combining eulliat jolis (1G),( 19), (20), and (21), we obtain

I

'

(due

du)2

dx ì(due;

du)2

tlx

2 j0

\dx

dx

2 j0

dx dx

f(g - G)

(--

dx

1L

(q Q)(u0

-.[f1_

G)2

+Q)2dx]1/2

r r (du0

du'\-Xl

I

1 --

I dx

[J0 \dx

cLr/

+ [f

L

(q -

Q)2d1/

[f (u0 -

tio)2dx]'.

(22)

Next, we consider outiv (lu-

left and right members of

t (te

in-equality of eqtration (22) and niake use of equation (18) to obtain tif

fu (du-

-Adx

lit' 2

\

dx drJ .

[

f (g - G)2

(pia

+

)2

(1.r]

[r-('

(/u)2

th E

r

i'

r

r1

¡du2, a0

\2

11/.

+ '

Li

t' - Q i dx]

[j

-

)

(IX]

rL

r

rL

la

du \ 2 o o (Ix

J

(U -

u0)2dx L \ dxq ) dx dx

dx,

lu getterai, tite fiuuirtittis

it(;( u satisfy tlitfereut ditTen-ittial

. /

2 eqiiat lotis; thus the expu-e-ittui of tue mean difference uf t lie

< ji

(

i

dx. (13) derivatives in equation (2) is

not zero ioud we can divido t hiough

\ dx

dx /

by it.

Also, since n0 atid

ti sat i'fv (lie respective clifferctttia!

/

(hiC

(Ill \

2

By returtiitig to equation (16), rearranging tite ieft-hnd lute- equations we know that

+

y")

is bounded above by 2If.

grais, unid niakiitg tise of tite Se.hwartz-Iltiitiakovsky intequalit.y

liv using these factswe obtain tite firmai iiiequalit y tif t his

in-we obtain the following expressions:

vest igation,

11L

(g - G)

(2

-

iix

[1L(th10

du)2

d.r]

<[.i13

1L

(g

G)2dÏ]'

=

f (g - G) (

+

(

-

) dx

+

2I

r

1L(q Q)2dx]/2 (24) <

i[

r

(g - G)2 (

+

ax

2LJo

dx dx

g, [j0

(23)

The inequality f equation

(24) elemoiistrates the meant cou-vergence of to as the fuinictionis G, Q approach g,

q, r

dx dx

(19) spectively.

By equation (17) we cani show uittifornt convergence of the displacements.

Discussion

Two fitta! expressiu)ns at-e needed to discuss the quest loti raised

(20) in the Introduction. These are obttiuted by ulsitug the triangle inequalities

ELf'

[j

i-J /

MARCH 1971

liarisactious of the ASME

<

1dudug

dx

-

(ix dx

dx

(4)

I- ti

(,r, -

1101 -f

iI; - u,l,

r ¡'

f(l(TR duQ 2 /J

j.!.

du\

'/2

Li0

!,,

dx -

ej;)

IIX]

[

¡

- -i;)

dx]

L (i

du,\2

2/3

+[Í

dx

I dx

dx/

]

(25)

13v contlittting equations(7)atol (24) with (25), we obtain

jUR

uI

()hí2

+

[(.

j.L

(g - G)2dx )'/z

+ 2L

(f (q -

Q)2i.r)]

wli it'h t bese ilpprt Ix iitt:tt ions are pari i cri larly mua ,rtttttt is shell

liti tlysis using vu ri ti jot ial pri n ripies. 'l'i re fu net h u tais associated

wit h shell problems are very complex, rer1ltirittg sittiplihittition of tine geometrical expressions itt t,rder to lie feasible for

program-ming.

The author thanks tite reviewer for suggest iltg that he indicate t lie existence of a ttrtrnber of pitblished papers ott tite subject of

hitnite-element couvergetice. Ile also expresses appreciatiott for

tite prompt reply oit the review. Acknowledgment

This work was supported by NASA N(ffi 46-001-008 S2 68-16. Tite author wiiìes to thank P. E. Grafton of the Boeing Company Aerospace Group fuir suggesting the research topic.

References

i Martin, H. C., Introduction to Matrix .tfethods of Strnct,iral

Analysis, McGraw-Hill, New York, 1966.

2 l'rzemieziietki, J. S., Theory f ,tfati'ix Striietiii'al Analyitt, McGraw-Hill, New York, 196S.

3 Guyan, R. J., 'Redurtiot, of Stillness and Mass Matrices," AJAA Journal, Vol. 3, No. 2, Feb. 11)65 j , 380.

4 MeLay, R. WC., 'An Investigatioti Lutto the Titeory of tite

Dis-liittiernent Method of Analysis for I.iue'rr Elasticity," Ihi) thesis, Department of Etigiticering Mer1itntic... Uutiversitv of "uVisconsin,

M:rdison, Wis., Aug. 1963.

5 Key, S. M., ('rnttvergeiuce Ittvc'stigation of the I)irect Stiff-ncr_Sn Methoil," PhD e-i., [)ettriiuietii of Aeronautics nuit

Astro-1trirttít'-, University of \Vashittgtoii, Serti Iv, \Vttsh., iInir. 1966.

Tong, I'., :triul l'ian, T. IL. IL., ''Tie ('onvergence of the

Finite-1']etiieri t Method itt Sitiviitg Li trt':t t 11 ;n r ir I 'rol ,lenis, '' fnternaiional Joirrno/ of Solûls and S!rnrlures, 'ol. 3, ltui7, pp. 865--879.

7 Birkoff, O., $n'}tultz, M. LI., iii Varga, R. S., 'Piecewise

lierntite interi,ol:iti,ri it, Otte and Two \':ti'iabies With Aptiications to I'artial Differenti:,! Eu:ttiotto," ,\'nim ,ische Mathemat'i/r, Voi. 1),

1968, p. 232 -256.

S Oliveira, E. it. A., ''Tlteoretic:tl i"oundations of tite Finite-Flettiert Met hod,'' I',tri',al ¡0/0/ .100 d i of .Soiitis and ,S'lr' wi ri's,

4, 1968, pp. 112U t t52.

9 Ii ulnte, B. L.. ''irrt ert ii: ti titi iv hit z A pproxi nation.'' Jour-nalo.fMat/rernatics a,'!.lJ,'e/nar,je.', Vol LS. 1968, pit. 337-342.

It) Johnson, M. \\'., J,'., 'riti MeLay, It. W'., "Convergence of the

Firnite-1'1ettient Metl>d jut lit, l'iteory f Elasticity,'' JOUIINAL OF

Ai't't.ii, MECHANICS, \'i,l. 35,TItANS.A*\EE, Vii. 90, Series E., No.

2, Joue 1968, iii. 274 278.

Ii Fix, G., and St rang, (t., ''Fourier Artal','sis of tite

Fittite-Ele-meint Methods in ltiiz-(i:tlerkin 'I'heory,'' .S/r,dies in App/ted Math-e-no/leS, \'ol. 48, No. 3. 191W, trI,. 26,'- 273.

r r'-

(dUR

du\

1''

fj[\l/2

I I I

- I

(lXi

I

-LJo

\dx

dx/

J

\2

Journal of Applied Mechanics

MARCH 1971 /61

+

L [eu

j.L

(g - G)hdx

+ 2L

(1L(q

-

Q)2dx)']

(26)

Equation (26) illustrates the uniform convergence of the Ritz

soluti, it U, to the exact solution Q and mean convergence of the first dcrivativei. Note that the qttili1 y tif tite solution depends on bot it the ¡tiimber of elemen i s it t e t tush n and on t he q tt;ilit y

of the approximate fioul jotis G tii,l ÇL We also see I hat tito funet i ut dGjdx need not converge t vEx. This property itf

i lie va 'ial i tital principle is used whet i we idealize each elemet ti in an antilysis t.o be constant in t lie ervs-setI it liai area and Young's

moduli s. In this case dG'dx = I) in each element.

Equal ion (26) suggest s t hut a cit isit citi formulation reip tires the qitility of the approximations of ('.', Q to lie uf theMil1i( order

as thai uf the straiti appriximul ivttt. l'itt siniplv, if strains :ite

approximated as piecewise ci;nt titi funv'i iuv t hen it is sufficient that G,Q also be piecewise cotisi uit finid ions.

Thi si udy of a rest ii'ied prtui luto sii uws t hat many approxi-niatiov rs made ott using variai ii teil pri i cip us are rig( rous, ai-thotigi tt hey do ifltl appear sit si tltel'li tiny. The knowledge of

titis is of practical import tinco to the analyst ; lie cati go so far as

to define fuori ions numet'itally in i he eqttatiotts of the Rit z

Cytaty

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