Unit 6 Plane Stress and Plane Strain [PDF]

but this is not exactly true. ⇒ INCONSISTENCY. Why? This is an idealized model and thus an approximation. There are, i

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MIT - 16.20

Fall, 2002

Unit 6

Plane Stress and Plane Strain

Readings:

T&G

8, 9, 10, 11, 12, 14, 15, 16

Paul A. Lagace, Ph.D.

Professor of Aeronautics & Astronautics

and Engineering Systems

Paul A. Lagace © 2001

MIT - 16.20

Fall, 2002

There are many structural configurations where we do not have to deal with the full 3-D case. • First let’s consider the models • Let’s then see under what conditions we can apply them

A. Plane Stress This deals with stretching and shearing of thin slabs. Figure 6.1 Representation of Generic Thin Slab

Paul A. Lagace © 2001

Unit 6 - p. 2

MIT - 16.20

Fall, 2002

The body has dimensions such that h >”??? … we’ll consider later) Since the body is basically “infinite” along z, the important loads are in the x - y plane (none in z) and do not change with z:

∂ ∂ = = 0 ∂z ∂y 3 This implies there is no gradient in displacement along z, so (excluding rigid body movement): u3 = w = 0 Equations of elasticity become: Equilibrium: Primary

∂σ11 ∂σ 21 + + f1 = 0 ∂y 2 ∂y1

Paul A. Lagace © 2001

∂σ12 ∂σ 22 + + f2 = 0 ∂y 2 ∂y1

(1)

(2) Unit 6 - p. 11

MIT - 16.20

Fall, 2002

Secondary ∂σ13 ∂σ 23 + + f3 = 0 ∂y 2 ∂y1 σ13 and σ23 exist but do not enter into primary consideration Strain - Displacement

ε11

=

∂u1 ∂y1

(3)

ε 22

=

∂u2 ∂y 2

(4)

=

∂u2  1  ∂u1 +   ∂y1  2  ∂y 2

ε12

(5)

  Assumptions  ∂ = 0, w = 0 give:  ∂y 3  ε13 = ε 23 = ε 33 = 0 (Plane strain) Paul A. Lagace © 2001

Unit 6 - p. 12

MIT - 16.20

Fall, 2002

Stress - Strain (Do a similar procedure as in plane stress) 3 Primary σ11 = ...

(6)

σ 22 = ...

(7)

σ12 = ...

(8)

Secondary

σ13 = 0 σ 23 = 0

orthotropic

(≠ 0 for anisotropic)

σ 33 ≠ 0 INCONSISTENCY: No load along z, yet σ33 (σzz) is non zero. Why? Once again, this is an idealization. Triaxial strains (ε 33) actually arise. You eliminate σ33 from the equation set by expressing it in terms of σαβ via (σ33) stress-strain equation. Paul A. Lagace © 2001

Unit 6 - p. 13

MIT - 16.20

Fall, 2002

SUMMARY

Plane Stress

Plane Strain

Geometry:

thickness (y3) > in-plane dimensions (y1, y2)

Loading:

σ33 Issues of scale • What am I using the answer for? at what level? • Example: standing on table --overall deflection or reactions in legs are not dependent on way I stand (tip toe or flat foot) Paul A. Lagace © 2001

Unit 6 - p. 17

MIT - 16.20

Fall, 2002

⇒ model of top of table as plate in bending is sufficient --stresses under my foot very sensitive to specifics (if table top is foam, the way I stand will determine whether or not I crush the foam) --> How “good” do I need the answer? • In preliminary design, need “ballpark” estimate; in final design, need “exact” numbers • Example: as thickness increases when is a plate no longer in plane stress

Paul A. Lagace © 2001

Unit 6 - p. 18

MIT - 16.20

Figure 6.7

Fall, 2002

Representation of the “continuum” from plane stress to plane strain

very thin a continuum (plane stress) very thick (plane strain)

No line(s) of demarkation. Numbers approach idealizations but never get to it.

Must use engineering judgment AND Clearly identify key assumptions in model and resulting limitations Paul A. Lagace © 2001

Unit 6 - p. 19

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