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Deformation (physics)

From Wikipedia, the free encyclopedia
Transformation of a body from a reference configuration to a current configuration
For usage in engineering, seeDeformation (engineering).
Deformation
The deformation of a thin straight rod into a closed loop. The length of the rod remains almost unchanged during the deformation, which indicates that the strain is small. In this particular case of bending, displacements associated with rigid translations and rotations of material elements in the rod are much greater than displacements associated with straining.
InSI base unitsm
DimensionL{\displaystyle {\mathsf {L}}}
Part of a series on
Continuum mechanics
J=Ddφdx{\displaystyle J=-D{\frac {d\varphi }{dx}}}

Inphysics andcontinuum mechanics,deformation is the change in theshape or size of an object. It hasdimension oflength withSI unit ofmetre (m). It is quantified as the residualdisplacement of particles in a non-rigid body, from aninitial configuration to afinal configuration, excluding the body's averagetranslation androtation (itsrigid transformation).[1] Aconfiguration is a set containing thepositions of all particles of the body.

A deformation can occur because ofexternal loads,[2] intrinsic activity (e.g.muscle contraction),body forces (such asgravity orelectromagnetic forces), or changes in temperature, moisture content, or chemical reactions, etc.

In acontinuous body, adeformation field results from astress field due to appliedforces or because of some changes in the conditions of the body. The relation between stress andstrain (relative deformation) is expressed byconstitutive equations, e.g.,Hooke's law forlinear elastic materials.

Deformations which cease to exist after the stress field is removed are termed aselastic deformation. In this case, the continuum completely recovers its original configuration. On the other hand, irreversible deformations may remain, and these exist even after stresses have been removed. One type of irreversible deformation isplastic deformation, which occurs in material bodies after stresses have attained a certain threshold value known as theelastic limit oryield stress, and are the result ofslip, ordislocation mechanisms at the atomic level. Another type of irreversible deformation isviscous deformation, which is the irreversible part ofviscoelastic deformation.In the case of elastic deformations, the response function linking strain to the deforming stress is thecompliance tensor of the material.

Definition and formulation

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Deformation is the change in the metric properties of a continuous body, meaning that a curve drawn in the initial body placement changes its length when displaced to a curve in the final placement. If none of the curves changes length, it is said that arigid body displacement occurred.

It is convenient to identify a reference configuration or initial geometric state of the continuum body which all subsequent configurations are referenced from. The reference configuration need not be one the body actually will ever occupy. Often, the configuration att = 0 is considered the reference configuration,κ0(B). The configuration at the current timet is thecurrent configuration.

For deformation analysis, the reference configuration is identified asundeformed configuration, and the current configuration asdeformed configuration. Additionally, time is not considered when analyzing deformation, thus the sequence of configurations between the undeformed and deformed configurations are of no interest.

The componentsXi of the position vectorX of a particle in the reference configuration, taken with respect to the reference coordinate system, are called thematerial or reference coordinates. On the other hand, the componentsxi of the position vectorx of a particle in the deformed configuration, taken with respect to the spatial coordinate system of reference, are called thespatial coordinates

There are two methods for analysing the deformation of a continuum. One description is made in terms of the material or referential coordinates, calledmaterial description or Lagrangian description. A second description of deformation is made in terms of the spatial coordinates it is called thespatial description or Eulerian description.

There is continuity during deformation of a continuum body in the sense that:

  • The material points forming a closed curve at any instant will always form a closed curve at any subsequent time.
  • The material points forming a closed surface at any instant will always form a closed surface at any subsequent time and the matter within the closed surface will always remain within.

Affine deformation

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Anaffine deformation is a deformation that can be completely described by anaffine transformation. Such a transformation is composed of alinear transformation (such as rotation, shear, extension and compression) and a rigid body translation. Affine deformations are also calledhomogeneous deformations.[3]

Therefore, an affine deformation has the formx(X,t)=F(t)X+c(t){\displaystyle \mathbf {x} (\mathbf {X} ,t)={\boldsymbol {F}}(t)\cdot \mathbf {X} +\mathbf {c} (t)}wherex is the position of a point in the deformed configuration,X is the position in a reference configuration,t is a time-like parameter,F is the linear transformer andc is the translation. In matrix form, where the components are with respect to an orthonormal basis,[x1(X1,X2,X3,t)x2(X1,X2,X3,t)x3(X1,X2,X3,t)]=[F11(t)F12(t)F13(t)F21(t)F22(t)F23(t)F31(t)F32(t)F33(t)][X1X2X3]+[c1(t)c2(t)c3(t)]{\displaystyle {\begin{bmatrix}x_{1}(X_{1},X_{2},X_{3},t)\\x_{2}(X_{1},X_{2},X_{3},t)\\x_{3}(X_{1},X_{2},X_{3},t)\end{bmatrix}}={\begin{bmatrix}F_{11}(t)&F_{12}(t)&F_{13}(t)\\F_{21}(t)&F_{22}(t)&F_{23}(t)\\F_{31}(t)&F_{32}(t)&F_{33}(t)\end{bmatrix}}{\begin{bmatrix}X_{1}\\X_{2}\\X_{3}\end{bmatrix}}+{\begin{bmatrix}c_{1}(t)\\c_{2}(t)\\c_{3}(t)\end{bmatrix}}}

The above deformation becomesnon-affine orinhomogeneous ifF =F(X,t) orc =c(X,t).

Rigid body motion

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A rigid body motion is a special affine deformation that does not involve any shear, extension or compression. The transformation matrixF isproper orthogonal in order to allow rotations but noreflections.

A rigid body motion can be described byx(X,t)=Q(t)X+c(t){\displaystyle \mathbf {x} (\mathbf {X} ,t)={\boldsymbol {Q}}(t)\cdot \mathbf {X} +\mathbf {c} (t)}whereQQT=QTQ=1{\displaystyle {\boldsymbol {Q}}\cdot {\boldsymbol {Q}}^{T}={\boldsymbol {Q}}^{T}\cdot {\boldsymbol {Q}}={\boldsymbol {\mathit {1}}}}In matrix form,[x1(X1,X2,X3,t)x2(X1,X2,X3,t)x3(X1,X2,X3,t)]=[Q11(t)Q12(t)Q13(t)Q21(t)Q22(t)Q23(t)Q31(t)Q32(t)Q33(t)][X1X2X3]+[c1(t)c2(t)c3(t)]{\displaystyle {\begin{bmatrix}x_{1}(X_{1},X_{2},X_{3},t)\\x_{2}(X_{1},X_{2},X_{3},t)\\x_{3}(X_{1},X_{2},X_{3},t)\end{bmatrix}}={\begin{bmatrix}Q_{11}(t)&Q_{12}(t)&Q_{13}(t)\\Q_{21}(t)&Q_{22}(t)&Q_{23}(t)\\Q_{31}(t)&Q_{32}(t)&Q_{33}(t)\end{bmatrix}}{\begin{bmatrix}X_{1}\\X_{2}\\X_{3}\end{bmatrix}}+{\begin{bmatrix}c_{1}(t)\\c_{2}(t)\\c_{3}(t)\end{bmatrix}}}

Background: displacement

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Main articles:Displacement (physics) andDisplacement field (mechanics)
Figure 1. Motion of a continuum body.

A change in the configuration of a continuum body results in adisplacement. The displacement of a body has two components: a rigid-body displacement and a deformation. A rigid-body displacement consists of a simultaneous translation and rotation of the body without changing its shape or size. Deformation implies the change in shape and/or size of the body from an initial or undeformed configurationκ0(B) to a current or deformed configurationκt(B) (Figure 1).

If after a displacement of the continuum there is a relative displacement between particles, a deformation has occurred. On the other hand, if after displacement of the continuum the relative displacement between particles in the current configuration is zero, then there is no deformation and a rigid-body displacement is said to have occurred.

The vector joining the positions of a particleP in the undeformed configuration and deformed configuration is called thedisplacement vectoru(X,t) =uiei in the Lagrangian description, orU(x,t) =UJEJ in the Eulerian description.

Adisplacement field is a vector field of all displacement vectors for all particles in the body, which relates the deformed configuration with the undeformed configuration. It is convenient to do the analysis of deformation or motion of a continuum body in terms of the displacement field. In general, the displacement field is expressed in terms of the material coordinates asu(X,t)=b(X,t)+x(X,t)Xorui=αiJbJ+xiαiJXJ{\displaystyle \mathbf {u} (\mathbf {X} ,t)=\mathbf {b} (\mathbf {X} ,t)+\mathbf {x} (\mathbf {X} ,t)-\mathbf {X} \qquad {\text{or}}\qquad u_{i}=\alpha _{iJ}b_{J}+x_{i}-\alpha _{iJ}X_{J}}or in terms of the spatial coordinates asU(x,t)=b(x,t)+xX(x,t)orUJ=bJ+αJixiXJ{\displaystyle \mathbf {U} (\mathbf {x} ,t)=\mathbf {b} (\mathbf {x} ,t)+\mathbf {x} -\mathbf {X} (\mathbf {x} ,t)\qquad {\text{or}}\qquad U_{J}=b_{J}+\alpha _{Ji}x_{i}-X_{J}}whereαJi are the direction cosines between the material and spatial coordinate systems with unit vectorsEJ andei, respectively. ThusEJei=αJi=αiJ{\displaystyle \mathbf {E} _{J}\cdot \mathbf {e} _{i}=\alpha _{Ji}=\alpha _{iJ}}and the relationship betweenui andUJ is then given byui=αiJUJorUJ=αJiui{\displaystyle u_{i}=\alpha _{iJ}U_{J}\qquad {\text{or}}\qquad U_{J}=\alpha _{Ji}u_{i}}

Knowing thatei=αiJEJ{\displaystyle \mathbf {e} _{i}=\alpha _{iJ}\mathbf {E} _{J}}thenu(X,t)=uiei=ui(αiJEJ)=UJEJ=U(x,t){\displaystyle \mathbf {u} (\mathbf {X} ,t)=u_{i}\mathbf {e} _{i}=u_{i}(\alpha _{iJ}\mathbf {E} _{J})=U_{J}\mathbf {E} _{J}=\mathbf {U} (\mathbf {x} ,t)}

It is common to superimpose the coordinate systems for the undeformed and deformed configurations, which results inb = 0, and the direction cosines becomeKronecker deltas:EJei=δJi=δiJ{\displaystyle \mathbf {E} _{J}\cdot \mathbf {e} _{i}=\delta _{Ji}=\delta _{iJ}}

Thus, we haveu(X,t)=x(X,t)Xorui=xiδiJXJ=xiXi{\displaystyle \mathbf {u} (\mathbf {X} ,t)=\mathbf {x} (\mathbf {X} ,t)-\mathbf {X} \qquad {\text{or}}\qquad u_{i}=x_{i}-\delta _{iJ}X_{J}=x_{i}-X_{i}}or in terms of the spatial coordinates asU(x,t)=xX(x,t)orUJ=δJixiXJ=xJXJ{\displaystyle \mathbf {U} (\mathbf {x} ,t)=\mathbf {x} -\mathbf {X} (\mathbf {x} ,t)\qquad {\text{or}}\qquad U_{J}=\delta _{Ji}x_{i}-X_{J}=x_{J}-X_{J}}

Displacement gradient tensor

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Main article:Displacement gradient tensor

The partial differentiation of the displacement vector with respect to the material coordinates yields thematerial displacement gradient tensorXu. Thus we have:u(X,t)=x(X,t)XXu=XxIXu=FI{\displaystyle {\begin{aligned}\mathbf {u} (\mathbf {X} ,t)&=\mathbf {x} (\mathbf {X} ,t)-\mathbf {X} \\\nabla _{\mathbf {X} }\mathbf {u} &=\nabla _{\mathbf {X} }\mathbf {x} -\mathbf {I} \\\nabla _{\mathbf {X} }\mathbf {u} &=\mathbf {F} -\mathbf {I} \end{aligned}}}orui=xiδiJXJ=xiXiuiXK=xiXKδiK{\displaystyle {\begin{aligned}u_{i}&=x_{i}-\delta _{iJ}X_{J}=x_{i}-X_{i}\\{\frac {\partial u_{i}}{\partial X_{K}}}&={\frac {\partial x_{i}}{\partial X_{K}}}-\delta _{iK}\end{aligned}}}whereF is thedeformation gradient tensor.

Similarly, the partial differentiation of the displacement vector with respect to the spatial coordinates yields thespatial displacement gradient tensorxU. Thus we have,U(x,t)=xX(x,t)xU=IxXxU=IF1{\displaystyle {\begin{aligned}\mathbf {U} (\mathbf {x} ,t)&=\mathbf {x} -\mathbf {X} (\mathbf {x} ,t)\\\nabla _{\mathbf {x} }\mathbf {U} &=\mathbf {I} -\nabla _{\mathbf {x} }\mathbf {X} \\\nabla _{\mathbf {x} }\mathbf {U} &=\mathbf {I} -\mathbf {F} ^{-1}\end{aligned}}}orUJ=δJixiXJ=xJXJUJxk=δJkXJxk{\displaystyle {\begin{aligned}U_{J}&=\delta _{Ji}x_{i}-X_{J}=x_{J}-X_{J}\\{\frac {\partial U_{J}}{\partial x_{k}}}&=\delta _{Jk}-{\frac {\partial X_{J}}{\partial x_{k}}}\end{aligned}}}

Examples

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Homogeneous (or affine) deformations are useful in elucidating the behavior of materials. Some homogeneous deformations of interest are

Linear or longitudinal deformations of long objects, such as beams and fibers, are calledelongation orshortening; derived quantities are therelative elongation and thestretch ratio.

Plane deformations are also of interest, particularly in the experimental context.

Volume deformation is a uniform scaling due to isotropiccompression; the relative volume deformation is calledvolumetric strain.

Plane deformation

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A plane deformation, also calledplane strain, is one where the deformation is restricted to one of the planes in the reference configuration. If the deformation is restricted to the plane described by the basis vectorse1,e2, thedeformation gradient has the formF=F11e1e1+F12e1e2+F21e2e1+F22e2e2+e3e3{\displaystyle {\boldsymbol {F}}=F_{11}\mathbf {e} _{1}\otimes \mathbf {e} _{1}+F_{12}\mathbf {e} _{1}\otimes \mathbf {e} _{2}+F_{21}\mathbf {e} _{2}\otimes \mathbf {e} _{1}+F_{22}\mathbf {e} _{2}\otimes \mathbf {e} _{2}+\mathbf {e} _{3}\otimes \mathbf {e} _{3}}In matrix form,F=[F11F120F21F220001]{\displaystyle {\boldsymbol {F}}={\begin{bmatrix}F_{11}&F_{12}&0\\F_{21}&F_{22}&0\\0&0&1\end{bmatrix}}}From thepolar decomposition theorem, the deformation gradient, up to a change of coordinates, can be decomposed into a stretch and a rotation. Since all the deformation is in a plane, we can write[3]F=RU=[cosθsinθ0sinθcosθ0001][λ1000λ20001]{\displaystyle {\boldsymbol {F}}={\boldsymbol {R}}\cdot {\boldsymbol {U}}={\begin{bmatrix}\cos \theta &\sin \theta &0\\-\sin \theta &\cos \theta &0\\0&0&1\end{bmatrix}}{\begin{bmatrix}\lambda _{1}&0&0\\0&\lambda _{2}&0\\0&0&1\end{bmatrix}}}whereθ is the angle of rotation andλ1,λ2 are theprincipal stretches.

Isochoric plane deformation

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If the deformation is isochoric (volume preserving) thendet(F) = 1 and we haveF11F22F12F21=1{\displaystyle F_{11}F_{22}-F_{12}F_{21}=1}Alternatively,λ1λ2=1{\displaystyle \lambda _{1}\lambda _{2}=1}

Simple shear

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Asimple shear deformation is defined as an isochoric plane deformation in which there is a set of line elements with a given reference orientation that do not change length and orientation during the deformation.[3]

Ife1 is the fixed reference orientation in which line elements do not deform during the deformation thenλ1 = 1 andF·e1 =e1.Therefore,F11e1+F21e2=e1F11=1 ;  F21=0{\displaystyle F_{11}\mathbf {e} _{1}+F_{21}\mathbf {e} _{2}=\mathbf {e} _{1}\quad \implies \quad F_{11}=1~;~~F_{21}=0}Since the deformation is isochoric,F11F22F12F21=1F22=1{\displaystyle F_{11}F_{22}-F_{12}F_{21}=1\quad \implies \quad F_{22}=1}Defineγ:=F12{\displaystyle \gamma :=F_{12}}Then, the deformation gradient in simple shear can be expressed asF=[1γ0010001]{\displaystyle {\boldsymbol {F}}={\begin{bmatrix}1&\gamma &0\\0&1&0\\0&0&1\end{bmatrix}}}Now,Fe2=F12e1+F22e2=γe1+e2F(e2e2)=γe1e2+e2e2{\displaystyle {\boldsymbol {F}}\cdot \mathbf {e} _{2}=F_{12}\mathbf {e} _{1}+F_{22}\mathbf {e} _{2}=\gamma \mathbf {e} _{1}+\mathbf {e} _{2}\quad \implies \quad {\boldsymbol {F}}\cdot (\mathbf {e} _{2}\otimes \mathbf {e} _{2})=\gamma \mathbf {e} _{1}\otimes \mathbf {e} _{2}+\mathbf {e} _{2}\otimes \mathbf {e} _{2}}Sinceeiei=1{\displaystyle \mathbf {e} _{i}\otimes \mathbf {e} _{i}={\boldsymbol {\mathit {1}}}}we can also write the deformation gradient asF=1+γe1e2{\displaystyle {\boldsymbol {F}}={\boldsymbol {\mathit {1}}}+\gamma \mathbf {e} _{1}\otimes \mathbf {e} _{2}}

See also

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References

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  1. ^Truesdell, C.; Noll, W. (2004).The non-linear field theories of mechanics (3rd ed.). Springer. p. 48.
  2. ^Wu, H.-C. (2005).Continuum Mechanics and Plasticity. CRC Press.ISBN 1-58488-363-4.
  3. ^abcOgden, R. W. (1984).Non-linear Elastic Deformations. Dover.

Further reading

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