Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

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6.8 Finite Element Method for Continuum Structures 199

Fig.6.13


Triangular element for plane elasticity problems.


thattheinverseofthe[A]matrixforatriangularelementcontainstermsgivingtheactualareaofthe
element;thisareaispositiveiftheprecedingnodeletteringornumberingsystemisadopted.Theele-
ment is to be used for plane elasticity problems and has therefore two degrees of freedom per node,
giving a total of six degrees of freedom for the element, which results in a 6×6 element stiffness
matrix[Ke].Thenodalforcesanddisplacementsareshown,andthecompletedisplacementandforce
vectorsare


{δe}=


⎪⎪

⎪⎪

⎪⎪

⎪⎪


⎪⎪

⎪⎪⎪

⎪⎪

⎪⎩

ui
vi
uj
vj
uk
vk


⎪⎪

⎪⎪

⎪⎪

⎪⎪


⎪⎪

⎪⎪⎪

⎪⎪

⎪⎭

{Fe}=


⎪⎪

⎪⎪

⎪⎪

⎪⎪


⎪⎪

⎪⎪⎪

⎪⎪

⎪⎩

Fx,i
Fy,i
Fx,j
Fy,j
Fx,k
Fy,k


⎪⎪

⎪⎪

⎪⎪

⎪⎪


⎪⎪

⎪⎪⎪

⎪⎪

⎪⎭

(6.81)

Wenowselectadisplacementfunctionwhichmustsatisfytheboundaryconditionsoftheelement—
that is, the condition that each node possesses two degrees of freedom. Generally, for computational
purposes, a polynomial is preferable to, say, a trigonometric series, since the terms in a polynomial
canbecalculatedmuchmorerapidlybyadigitalcomputer.Furthermore,thetotalnumberofdegrees
of freedom is six so that only six coefficients in the polynomial can be obtained. Suppose that the
displacementfunctionis


u(x,y)=α 1 +α 2 x+α 3 y
v(x,y)=α 4 +α 5 x+α 6 y

}

(6.82)

Theconstantterms,α 1 andα 4 ,arerequiredtorepresentanyin-planerigidbodymotion—thatis,motion
withoutstrain—whilethelineartermsenablestatesofconstantstraintobespecified;Eqs.(6.82)ensure

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