Nobody Asked What Happens Sideways

Three sections in a row have been about one number changing. Section 4 stretched a wire and measured ΔL\Delta L. Section 5 sheared a block and measured the angle. Section 6 squeezed a cube and measured ΔV\Delta V.

Go back to the stretched wire for a moment. You pulled it, it got longer by ΔL\Delta L, and you computed Y=FLAΔLY = \frac{FL}{A\,\Delta L} and moved on. But something else happened at the same instant, and we have been quietly ignoring it.

The wire also got thinner.

Of course it did. Stretch a rubber band between your fingers and watch it — it narrows visibly. A steel wire does exactly the same thing; the change is just far too small to see. That sideways shrinking is a real, measurable, material-specific effect, and this section is about the number that measures it.

Rod stretched lengthways thins sideways, with the sign ledger for Poissons ratio

Lateral strain

The strain we have been using all along, ΔLL\frac{\Delta L}{L}, is the longitudinal strain — the fractional change along the direction you pulled. Now define its partner.

Key Point — lateral strain: Lateral strain is the fractional change in a dimension measured at right angles to the applied force. For a wire of diameter dd that thins by Δd\Delta d, lateral strain=Δdd\text{lateral strain} = \frac{\Delta d}{d} It is a strain like any other: a pure number, no unit, no dimensions. For a stretched wire it is negative, because Δd\Delta d is negative — the wire gets thinner while it gets longer.

Two details worth pinning down straight away.

  • It does not matter which transverse direction you pick. For an isotropic material the wire shrinks by the same fraction in every direction perpendicular to the pull. Diameter, radius, width, breadth — the fractional change is the same number. That is why you may safely write Δdd=Δrr\frac{\Delta d}{d} = \frac{\Delta r}{r} and use whichever the question gives you.
  • Compress instead of stretching and every sign flips. Squash a rod and it gets shorter and fatter: ΔLL\frac{\Delta L}{L} is negative and Δdd\frac{\Delta d}{d} is positive. The two are still opposite in sign, which is the whole point.

Poisson's ratio

Experiment shows something rather beautiful: for a given material, over the range where Hooke's law holds, the two strains are in a fixed ratio. Double the load and both strains double; their quotient does not budge.

Key Point — Poisson's ratio: Poisson's ratio is the negative of the ratio of lateral strain to longitudinal strain: σ=lateral strainlongitudinal strain=Δd/dΔL/L\sigma = -\frac{\text{lateral strain}}{\text{longitudinal strain}} = -\frac{\Delta d/d}{\Delta L/L} It is dimensionless and has no unit, being a ratio of two pure numbers. It is a property of the material, not of the particular specimen — its length and thickness cancel out of the definition entirely.

Why the minus sign is there — say this, every time

This is the same kind of sign question as the one in the bulk modulus, and it has the same kind of answer.

For an ordinary material the two strains always have opposite signs: pull it and ΔLL>0\frac{\Delta L}{L} > 0 while Δdd<0\frac{\Delta d}{d} < 0. Their quotient is therefore a negative number. If we defined Poisson's ratio as that quotient, every ordinary material would have a negative σ\sigma, and we would spend the rest of our lives carrying a minus sign around for no reason.

Key Point: The minus sign in the definition exists so that σ\sigma comes out positive for ordinary materials. It is a bookkeeping choice, exactly like the minus sign in B=ΔpΔV/VB = -\frac{\Delta p}{\Delta V/V}, and it earns a mark in a definition question. Write it, and say what it is for.

A useful rearrangement, which is what you actually use in problems:

Δdd=σΔLLΔd=σdΔLL\frac{\Delta d}{d} = -\sigma\,\frac{\Delta L}{L} \qquad\Longrightarrow\qquad \lvert \Delta d \rvert = \sigma\, d\, \frac{\Delta L}{L}

So if you know σ\sigma and you know how much the wire stretched, you know exactly how much thinner it got.

The symbol, at last

σ\sigma means Poisson's ratio, and stress is written FA\frac{F}{A} or σL\sigma_L, σs\sigma_s, σh\sigma_h when a symbol is genuinely needed. This is the section where that reservation finally pays for itself. Elsewhere σ\sigma often denotes stress, with ν\nu (nu) or μ\mu (mu) for Poisson's ratio — check the symbol list first and do not mix the two conventions inside a single solution.

[Board Important] "Define Poisson's ratio. Why is a negative sign used in its definition?" is a standard two-mark question. One mark for the ratio, one for the sentence about the sign. Adding "it is dimensionless and has no unit" costs you nothing and often picks up the third mark in a three-mark version.

What a Stretched Rod Does to Its Own Volume

Here is a question that sounds harmless and catches almost everybody: when you stretch a wire, does its volume go up, go down, or stay the same?

Think about the two competing effects. The wire gets longer, which increases the volume. It also gets thinner, which decreases it. Which wins?

Let us just do the sum. It takes two lines.

The two-line derivation

Take a rod of length LL and square cross-section of side aa, so that V=a2LV = a^{2}L. (A circular wire gives exactly the same answer — try it as an exercise.) Stretch it. The length gains a fraction ΔLL\frac{\Delta L}{L}; each of the two transverse sides loses a fraction σΔLL\sigma\frac{\Delta L}{L}.

For small changes, fractional changes simply add:

ΔVV=ΔLL+2Δaa\frac{\Delta V}{V} = \frac{\Delta L}{L} + 2\,\frac{\Delta a}{a}

That factor of 2 is the whole trick and the whole trap. There is one length and there are two transverse dimensions, and both of them shrink. Now substitute Δaa=σΔLL\frac{\Delta a}{a} = -\sigma\frac{\Delta L}{L}:

Key Point — the volume change of a stretched rod: ΔVV=ΔLL2σΔLL=(12σ)ΔLL\frac{\Delta V}{V} = \frac{\Delta L}{L} - 2\sigma\frac{\Delta L}{L} = (1 - 2\sigma)\,\frac{\Delta L}{L} This holds for small strains and for an isotropic material. It works for a wire, a rod, a bar of any cross-section.

Stretched bar volume change and the straight line one minus two sigma

Reading the answer off

Everything now depends on the single factor (12σ)(1 - 2\sigma):

  • σ<0.5\sigma < 0.5 — then (12σ)>0(1 - 2\sigma) > 0 and the volume increases. Since every ordinary metal has σ\sigma between 0.20.2 and 0.450.45, this is the normal case. Stretching a steel wire makes it very slightly bigger.
  • σ=0.5\sigma = 0.5 — then (12σ)=0(1 - 2\sigma) = 0 and the volume does not change at all. The lengthening and the thinning cancel exactly. Such a material is called incompressible, and rubber comes extremely close to it.
  • σ>0.5\sigma > 0.5 — the volume would decrease when you pulled it. No material does this, and the next block explains why it cannot.

Key Point: σ=0.5\sigma = 0.5 is precisely the value at which a stretched body conserves its volume. Not approximately — exactly, to first order. Whenever a question says "the material is incompressible" or "the volume remains constant on stretching", it has just handed you σ=0.5\sigma = 0.5.

How good is "for small changes"? Let us check rather than assume

That phrase "fractional changes simply add" is an approximation, and this chapter does not let approximations pass unexamined. So compute the exact new volume by multiplying out the real deformed dimensions,

VV=(1+ε)(1σε)2\frac{V^{\,\prime}}{V} = (1 + \varepsilon)\,(1 - \sigma\varepsilon)^{2}

and compare it with the linear answer (12σ)ε(1-2\sigma)\varepsilon. Here is what comes out:

Longitudinal strain ε\varepsilon σ\sigma Exact ΔVV\frac{\Delta V}{V} Linear (12σ)ε(1-2\sigma)\varepsilon Error of the linear form
1×1041 \times 10^{-4} 0.29 4.1995×1054.1995 \times 10^{-5} 4.2000×1054.2000 \times 10^{-5} 0.01%
1×1031 \times 10^{-3} 0.29 4.1950×1044.1950 \times 10^{-4} 4.2000×1044.2000 \times 10^{-4} 0.12%
1×1021 \times 10^{-2} 0.29 4.1505×1034.1505 \times 10^{-3} 4.2000×1034.2000 \times 10^{-3} 1.2%
5×1025 \times 10^{-2} 0.40 8.4200×1038.4200 \times 10^{-3} 1.0000×1021.0000 \times 10^{-2} 18.8%
1×1011 \times 10^{-1} 0.40 1.3760×1021.3760 \times 10^{-2} 2.0000×1022.0000 \times 10^{-2} 45.3%

Exact deformed volume against the linearised formula. The exact column was obtained by multiplying the actual new dimensions together. As everywhere in this chapter, the error is measured against the exact value: linearexactexact×100\frac{\lvert \text{linear} - \text{exact} \rvert}{\lvert \text{exact} \rvert} \times 100.

Read that table honestly. At the strains a metal actually works at — a few parts in ten thousand — the linear formula is good to better than a tenth of a per cent, and you should use it without a second thought. At rubber strains, where ε\varepsilon is measured in tens of per cent, the linear formula is out by nearly a half and is simply the wrong tool. That is not a defect in the physics; it is the visible edge of the small-strain assumption that the whole chapter rests on.

[JEE Tip] The single most common slip here is dropping the 2. Students write ΔVV=(1σ)ΔLL\frac{\Delta V}{V} = (1-\sigma)\frac{\Delta L}{L} because they counted one transverse direction instead of two. If you ever forget, rebuild it: one length, two widths, so one plus and two minuses.

How Big Is σ\sigma, and How Big Is It Allowed to Be?

Poisson's ratio is a pure number, so the question "how big is it?" has a clean answer. Here are real values.

Material Poisson's ratio σ\sigma
Cork about 0.0
Concrete 0.15 to 0.20
Glass 0.22
Cast iron 0.25
Steel 0.28 to 0.30
Iron 0.29
Aluminium 0.33
Copper 0.34
Brass 0.35
Titanium 0.36
Gold 0.42
Lead 0.44
Rubber 0.4999, effectively 0.5

Poisson's ratio for common materials. This is our own reference list for the chapter; use these values whenever a problem does not supply its own.

Key Point — the number to carry in your head: for ordinary metals, σ\sigma lies between about 0.2 and 0.45, and a typical value is around 0.3. If a calculation hands you σ=2.4\sigma = 2.4 or σ=0.03\sigma = 0.03 for a metal, you have made an arithmetic mistake, not a discovery.

Number line of Poissons ratio bounds with real materials marked on it

The theoretical bounds

The measured values all sit inside a window, and the window is not an accident of which materials happen to exist. It is forced by physics.

Key Point — the bounds on Poisson's ratio: 1σ0.5-1 \leq \sigma \leq 0.5 No isotropic material can have a value outside this range, whatever it is made of.

Where do the two ends come from? Each one is a modulus refusing to be negative. The relations that make this precise are set up in the next block, but the argument is short enough to give now.

  • The upper bound, σ0.5\sigma \leq 0.5. The next block derives Y=3B(12σ)Y = 3B(1 - 2\sigma). Both YY and BB must be positive — a material with a negative bulk modulus would expand when you squeezed it, gaining energy from nothing. Positive YY and positive BB force (12σ)>0(1 - 2\sigma) > 0, that is, σ<0.5\sigma < 0.5. At exactly 0.50.5, BB becomes infinite: the material is perfectly incompressible.
  • The lower bound, σ1\sigma \geq -1. The next block also gives Y=2G(1+σ)Y = 2G(1 + \sigma). Positive YY and positive GG force (1+σ)>0(1 + \sigma) > 0, that is, σ>1\sigma > -1. At exactly 1-1, GG becomes infinite: the material would resist shearing absolutely.

So the two bounds are simply the two moduli insisting on being positive. Nothing was measured to obtain them.

What the special values mean physically

  • σ=0\sigma = 0. Stretch it and it does not get thinner at all. Cork is very close to this, which is exactly why a cork goes into a bottleneck: push it in and it does not bulge sideways to jam. A rubber stopper of the same size would.
  • σ=0.5\sigma = 0.5. Volume exactly conserved, as the last block showed. Rubber, and most liquids-like solids and biological tissue, sit near here.
  • σ<0\sigma < 0. Stretch it and it gets fatter. Materials that do this are called auxetic. They are not found in ordinary metals; they are engineered — certain foams, folded structures and some crystals cut in particular directions. Their existence is why the lower bound is stated at 1-1 rather than at 00.

One caution about "isotropic"

Every statement in this section — the bounds, the relations in the next block, the claim that the lateral shrinkage is the same in all transverse directions — assumes the material is isotropic: the same in every direction. Ordinary metals, glass and most engineering materials are close enough for our purposes. Wood is not, and neither is a single crystal, and neither is carbon fibre. Wood cut along the grain behaves completely differently from wood cut across it, and for such materials Poisson's ratio is not a single number at all. That is well past Class 11, but it is worth knowing the assumption is there.

[NEET Important] Three one-liners that get asked directly: σ\sigma is dimensionless; its practical range for metals is 0.2 to 0.45; its theoretical range is 1-1 to 0.50.5. Options offering σ=0.6\sigma = 0.6, σ=1.0\sigma = 1.0 or σ=1.5\sigma = -1.5 for a real material are always wrong.

Tying All Four Constants Together

This block sits outside the rationalised syllabus body text, but JEE Main, JEE Advanced and NEET use these relations freely every year, so they are developed here from first principles.

We now have four numbers that describe how an elastic solid responds: YY, GG, BB and σ\sigma. They arrived in four different sections from four different experiments, and so far nothing has connected them.

They are connected. In fact, for an isotropic solid, only two of the four are independent — fix any two and the other two are determined. Here is why.

Four elastic constants linked by relations, and three routes to sigma compared

Deriving Y=3B(12σ)Y = 3B(1 - 2\sigma)

This one you can do yourself, and it uses only what is already on this page.

Take a cube and put it under a uniform pressure pp — a hydraulic stress. That is the same thing as applying a compressive stress of size pp along the xx axis, and along the yy axis, and along the zz axis, all at once. Strains from separate stresses simply add, so work out the strain along xx by counting three contributions:

  1. The compression along xx itself produces a strain pY-\frac{p}{Y}.
  2. The compression along yy squeezes the cube in the yy direction, so by Poisson's effect the cube expands along xx by +σpY+\sigma\frac{p}{Y}.
  3. The compression along zz does exactly the same: +σpY+\sigma\frac{p}{Y}.

Add them:

εx=pY+σpY+σpY=pY(12σ)\varepsilon_x = -\frac{p}{Y} + \sigma\frac{p}{Y} + \sigma\frac{p}{Y} = -\frac{p}{Y}\,(1 - 2\sigma)

By symmetry εy\varepsilon_y and εz\varepsilon_z are the same, and for small strains the volume strain is their sum:

ΔVV=εx+εy+εz=3pY(12σ)\frac{\Delta V}{V} = \varepsilon_x + \varepsilon_y + \varepsilon_z = -\frac{3p}{Y}(1 - 2\sigma)

Finally use the definition of the bulk modulus from Section 6, B=pΔV/VB = -\frac{p}{\Delta V/V}:

B=Y3(12σ)Y=3B(12σ)B = \frac{Y}{3(1 - 2\sigma)} \qquad\Longleftrightarrow\qquad Y = 3B\,(1 - 2\sigma)

Notice that the minus signs have all cancelled and BB has come out positive, exactly as Section 6 promised.

Y=2G(1+σ)Y = 2G(1 + \sigma)

The shear relation is proved the same way, but it needs one extra idea: a pure shear is the same stress state as a tension along one 45°45° diagonal together with an equal compression along the other. Set that up, work out the strains of the two diagonals with the same superposition trick, and the shear strain drops out. The construction is a little beyond Class 11 geometry, so we state the result and use it:

Y=2G(1+σ)G=Y2(1+σ)Y = 2G\,(1 + \sigma) \qquad\Longleftrightarrow\qquad G = \frac{Y}{2(1 + \sigma)}

The other two, by elimination

Now you have two equations in the four unknowns. Eliminate whichever quantity you do not want.

Eliminate YY by setting 3B(12σ)=2G(1+σ)3B(1-2\sigma) = 2G(1+\sigma) and solving for σ\sigma:

3B6Bσ=2G+2Gσ    3B2G=σ(6B+2G)3B - 6B\sigma = 2G + 2G\sigma \;\Longrightarrow\; 3B - 2G = \sigma(6B + 2G)

 σ=3B2G2(3B+G) \boxed{\ \sigma = \frac{3B - 2G}{2(3B + G)}\ }

Eliminate σ\sigma instead. From the first relation σ=12(1Y3B)\sigma = \frac{1}{2}\left(1 - \frac{Y}{3B}\right); from the second σ=Y2G1\sigma = \frac{Y}{2G} - 1. Set them equal and tidy up:

9Y=3G+1BY=9BG3B+G\frac{9}{Y} = \frac{3}{G} + \frac{1}{B} \qquad\Longleftrightarrow\qquad Y = \frac{9BG}{3B + G}

That last form is worth memorising in the 9Y\frac{9}{Y} shape rather than the 9BG3B+G\frac{9BG}{3B+G} shape — it is far easier to remember, and it looks pleasingly like the formula for resistors in parallel.

Key Point — the four relations, all together: Y=3B(12σ)Y=2G(1+σ)Y = 3B(1 - 2\sigma) \qquad\qquad Y = 2G(1 + \sigma) σ=3B2G2(3B+G)9Y=3G+1B\sigma = \frac{3B - 2G}{2(3B + G)} \qquad\qquad \frac{9}{Y} = \frac{3}{G} + \frac{1}{B} Any two of YY, GG, BB, σ\sigma determine the other two. An isotropic solid therefore has exactly two independent elastic constants, not four.

Which one to reach for

You are given You want Use
YY and σ\sigma BB B=Y3(12σ)B = \dfrac{Y}{3(1-2\sigma)}
YY and σ\sigma GG G=Y2(1+σ)G = \dfrac{Y}{2(1+\sigma)}
YY and GG σ\sigma σ=Y2G1\sigma = \dfrac{Y}{2G} - 1
YY and BB σ\sigma σ=12(1Y3B)\sigma = \dfrac{1}{2}\left(1 - \dfrac{Y}{3B}\right)
GG and BB σ\sigma σ=3B2G2(3B+G)\sigma = \dfrac{3B-2G}{2(3B+G)}
GG and BB YY 9Y=3G+1B\dfrac{9}{Y} = \dfrac{3}{G} + \dfrac{1}{B}

Six routes, two relations. Every row is one of the two boxed formulas, rearranged.

A promise from Section 5, finally kept

Section 5 noted that GG is empirically about 0.350.35 to 0.420.42 times YY for real metals, and said the reason would appear here. Now it can. Rearranged, the shear relation says

GY=12(1+σ)\frac{G}{Y} = \frac{1}{2(1 + \sigma)}

Put σ=0.20\sigma = 0.20 into that and you get 0.4170.417. Put σ=0.45\sigma = 0.45 in and you get 0.3450.345. So the observed band 0.3450.345 to 0.4170.417 is not an empirical curiosity at all — it is exactly what the metals' Poisson ratios of 0.20.2 to 0.450.45 force it to be. The rough rule "GY3G \approx \frac{Y}{3}" corresponds to σ=0.5\sigma = 0.5, which is why it always runs a little low for a real metal.

[JEE Tip] These relations turn a two-unknown problem into a one-unknown problem. "Given YY and σ\sigma, find the fractional volume change under a pressure pp" looks like it needs BB, which you were not given. It does not: compute BB from YY and σ\sigma in one line and carry on.

Do These Relations Actually Work? An Honest Test

The four relations are exact — for a perfectly isotropic, homogeneous, linearly elastic solid. Real metals are none of those things exactly. So before you trust the formulas on real data, let us test them on real data.

Here is the experiment. Take the chapter's own tabulated YY, GG and BB for six materials, all measured independently. Then compute Poisson's ratio three different ways — from YY and GG, from YY and BB, and from GG and BB. If the material were perfectly isotropic and the numbers were perfectly measured, all three would agree exactly.

Material YY (GPa) GG (GPa) BB (GPa) σ\sigma from Y,GY,G σ\sigma from Y,BY,B σ\sigma from G,BG,B YY predicted from G,BG,B Error in YY
Steel 200 84 160 0.190 0.292 0.277 215 +7.2%+7.2\%
Copper 120 42 140 0.429 0.357 0.364 114 4.5%-4.5\%
Iron 190 70 100 0.357 0.183 0.216 170 10.4%-10.4\%
Aluminium 70 25 72 0.400 0.338 0.344 67 4.0%-4.0\%
Brass 91 36 61 0.264 0.251 0.253 90 0.8%-0.8\%
Glass 65 23 37 0.413 0.207 0.243 57 12.1%-12.1\%

The relations tested against independently measured moduli. The last column compares Y=9BG3B+GY = \frac{9BG}{3B+G} with the measured YY.

The verdict, stated plainly

The agreement is good but not exact. Across these six materials, YY predicted from GG and BB lands within 0.8%0.8\% for brass, within about 4%4\% for copper and aluminium, about 7%7\% for steel, and around 1010 to 12%12\% for iron and glass. The average error in magnitude is about 6.5%6.5\%.

The three routes to σ\sigma scatter by a similar amount. For brass they agree beautifully — 0.2640.264, 0.2510.251, 0.2530.253. For steel they range from 0.1900.190 to 0.2920.292, and for glass from 0.2070.207 to 0.4130.413.

Key Point: The inter-constant relations are exact for an ideal isotropic solid and good to roughly ten per cent on real tabulated data. Do not expect a handbook's YY, GG and BB for the same metal to satisfy them to three figures. They will not.

Why the disagreement, and why it does not matter for you

Four honest reasons:

  1. Real metals are polycrystalline, made of countless tiny crystals, each of which is anisotropic. The bulk material is only approximately isotropic, and how approximately depends on how it was rolled, drawn or cast.
  2. "Steel" is not one material. Nor is "brass" or "glass". Each is a family of alloys and compositions whose moduli differ by several per cent from one another. The YY in a table and the BB in a different table may not even be the same alloy.
  3. The three moduli are measured by three different experiments, each with its own systematic error, on three different specimens.
  4. The table values are rounded to two significant figures. Rounding 8484 from a true 79.379.3 is already a 6%6\% change, and that alone moves σ\sigma from Y,GY,G from 0.260.26 to 0.190.19.

None of this makes the relations useless. It makes them what they are: exact statements about an idealised material, and good estimates for a real one.

For your exams the practical consequence is simple and worth stating clearly:

  • Inside a problem, treat the relations as exact. If a question gives you YY and σ\sigma and asks for BB, there is one right answer and you compute it. Examiners construct such questions from consistent numbers.
  • Comparing against a table, expect a ten per cent discrepancy and do not panic. If your computed GG for steel comes out as 7.75×10107.75 \times 10^{10} Pa while the table says 8.4×10108.4 \times 10^{10} Pa, nothing has gone wrong.

[Board Important] If a question asks you to "verify the relation" using tabulated data, the expected answer says the two sides agree to within experimental error, and names a reason — real materials are not perfectly isotropic. An answer claiming exact agreement to four figures is claiming something false.

Pulling the Section Together

The whole thing on one page

Quantity Formula Notes
Lateral strain Δdd\dfrac{\Delta d}{d} negative when the body is stretched
Poisson's ratio σ=Δd/dΔL/L\sigma = -\dfrac{\Delta d/d}{\Delta L/L} dimensionless; the minus sign makes σ>0\sigma > 0
Lateral change Δd=σdΔLL\lvert \Delta d \rvert = \sigma\, d\, \dfrac{\Delta L}{L} the working form
Volume change ΔVV=(12σ)ΔLL\dfrac{\Delta V}{V} = (1 - 2\sigma)\dfrac{\Delta L}{L} small strains, isotropic body
Practical range 0.20.2 to 0.450.45 for metals typical value about 0.30.3
Theoretical bounds 1σ0.5-1 \leq \sigma \leq 0.5 from G>0G > 0 and B>0B > 0
Incompressible σ=0.5\sigma = 0.5 volume exactly conserved
Bulk relation Y=3B(12σ)Y = 3B(1 - 2\sigma) derive it by superposing three stresses
Shear relation Y=2G(1+σ)Y = 2G(1 + \sigma) equivalently G=Y2(1+σ)G = \dfrac{Y}{2(1+\sigma)}
σ\sigma from GG and BB σ=3B2G2(3B+G)\sigma = \dfrac{3B - 2G}{2(3B + G)} eliminate YY
YY from GG and BB 9Y=3G+1B\dfrac{9}{Y} = \dfrac{3}{G} + \dfrac{1}{B} remember it in this shape
Independent constants two for any isotropic solid

Everything in Section 7, in one table. The last five rows sit outside the rationalised syllabus body text and are asked every year.

The six traps

  1. Dropping the 2. ΔVV=(12σ)ΔLL\frac{\Delta V}{V} = (1-2\sigma)\frac{\Delta L}{L}, not (1σ)(1-\sigma). One length, two widths.
  2. Losing the minus sign in the definition, and then reporting a negative Poisson's ratio for steel.
  3. Using diameter where the problem gave radius, or the other way round. It does not matter — the fractional change is the same either way — but students often convert unnecessarily and slip.
  4. Mixing conventions between books. If a source writes σ\sigma for stress, its Poisson's ratio is ν\nu or μ\mu. Decide which convention the question uses before you substitute.
  5. Forgetting that σ\sigma has no units. It is a ratio of two dimensionless strains. Answers in pascal are wrong by construction.
  6. Quoting σ>0.5\sigma > 0.5. If a calculation produces 0.70.7, the arithmetic is wrong. The bound is not a guideline.

A checking habit worth building

Whenever you compute one elastic constant from two others, check the answer against the plausible range before writing it down:

  • σ\sigma between 0.20.2 and 0.450.45 for a metal.
  • GG between about Y3\frac{Y}{3} and Y2.4\frac{Y}{2.4}.
  • BB of the same order as YY for a metal — usually somewhat smaller for steel, somewhat larger for copper.

A σ\sigma of 1.71.7 or a GG larger than YY tells you instantly that a substitution went in upside down, and it costs three seconds to look.

What comes next

You now have every static elastic constant this chapter defines. Section 8 asks the next obvious question: where does the work you did in stretching the wire actually go? The answer is a stored energy, and it comes with a factor of one half that catches more students than anything else in the chapter.

Solved Examples

Values used throughout this section, unless a problem supplies its own: Ysteel=2.0×1011Y_{\text{steel}} = 2.0 \times 10^{11} Pa, Ycopper=1.2×1011Y_{\text{copper}} = 1.2 \times 10^{11} Pa, Yaluminium=0.70×1011Y_{\text{aluminium}} = 0.70 \times 10^{11} Pa, σsteel=0.29\sigma_{\text{steel}} = 0.29, σcopper=0.34\sigma_{\text{copper}} = 0.34, σaluminium=0.33\sigma_{\text{aluminium}} = 0.33.

Example 1: How much thinner does the wire get?

A copper wire of diameter 2.0 mm is stretched until its length increases by 0.10%. Taking σ=0.34\sigma = 0.34 for copper, find the change in its diameter.

Solution:

  1. Write down the longitudinal strain. An increase of 0.10% means ε=ΔLL=0.0010=1.0×103\varepsilon = \frac{\Delta L}{L} = 0.0010 = 1.0 \times 10^{-3}

  2. Use the definition, rearranged. Δdd=σΔLL=0.34×1.0×103=3.4×104\frac{\Delta d}{d} = -\sigma\,\frac{\Delta L}{L} = -0.34 \times 1.0 \times 10^{-3} = -3.4 \times 10^{-4}

  3. Multiply by the actual diameter. With d=2.0d = 2.0 mm =2.0×103= 2.0 \times 10^{-3} m, Δd=3.4×104×2.0×103=6.8×107 m\Delta d = -3.4 \times 10^{-4} \times 2.0 \times 10^{-3} = -6.8 \times 10^{-7} \text{ m}

  4. Read the sign. The negative sign says the diameter decreased, which is what stretching does.

Final Answer: The diameter falls by 6.8×1076.8 \times 10^{-7} m, that is 0.68 micrometre. The new diameter is 1.99932 mm.

Takeaway: The lateral change is tiny because the longitudinal change is tiny, and σ\sigma is less than one. A wire stretched by a tenth of a per cent thins by only three hundredths of a per cent — which is exactly why nobody noticed it in Sections 4 to 6.

Example 2: Reading Poisson's ratio off a measurement

A wire 2.50 m long and 1.20 mm in diameter is loaded. Its length increases by 1.50 mm and its diameter falls by 0.288 micrometre. Find Poisson's ratio for the material.

Solution:

  1. Longitudinal strain. ΔLL=1.50×1032.50=6.00×104\frac{\Delta L}{L} = \frac{1.50 \times 10^{-3}}{2.50} = 6.00 \times 10^{-4}

  2. Lateral strain, keeping the sign: Δdd=0.288×1061.20×103=2.40×104\frac{\Delta d}{d} = \frac{-0.288 \times 10^{-6}}{1.20 \times 10^{-3}} = -2.40 \times 10^{-4}

  3. Take the ratio and put the minus sign in front. σ=2.40×1046.00×104=0.400\sigma = -\frac{-2.40 \times 10^{-4}}{6.00 \times 10^{-4}} = 0.400

  4. Sanity check. 0.4000.400 sits comfortably inside the metal band of 0.2 to 0.45. Plausible.

Final Answer: σ=0.400\sigma = 0.400

Takeaway: Neither the length nor the diameter of the wire appears in the answer. They cancelled when the strains were formed. That is the whole reason σ\sigma is a property of the material rather than of the specimen.

Example 3: The volume of a stretched steel rod

A steel rod of length 1.0 m and radius 5.0 mm is stretched with a force that produces a longitudinal strain of 1.0×1031.0 \times 10^{-3}. Take Y=2.0×1011Y = 2.0 \times 10^{11} Pa and σ=0.29\sigma = 0.29. Find (a) the stretching force, (b) the fractional change in volume, and (c) the actual change in volume.

Solution:

  1. (a) The force. The cross-section is A=πr2=π(5.0×103)2=7.854×105 m2A = \pi r^{2} = \pi (5.0 \times 10^{-3})^{2} = 7.854 \times 10^{-5} \text{ m}^2 and since FA=Yε\frac{F}{A} = Y\varepsilon, F=YAε=2.0×1011×7.854×105×1.0×103=1.571×104 NF = Y A \varepsilon = 2.0 \times 10^{11} \times 7.854 \times 10^{-5} \times 1.0 \times 10^{-3} = 1.571 \times 10^{4} \text{ N}

  2. (b) Fractional volume change. ΔVV=(12σ)ΔLL=(10.58)×1.0×103=4.2×104\frac{\Delta V}{V} = (1 - 2\sigma)\frac{\Delta L}{L} = (1 - 0.58) \times 1.0 \times 10^{-3} = 4.2 \times 10^{-4}

  3. (c) Actual volume change. The original volume is V=AL=7.854×105×1.0=7.854×105 m3V = A L = 7.854 \times 10^{-5} \times 1.0 = 7.854 \times 10^{-5} \text{ m}^3 ΔV=4.2×104×7.854×105=3.30×108 m3=0.033 cm3\Delta V = 4.2 \times 10^{-4} \times 7.854 \times 10^{-5} = 3.30 \times 10^{-8} \text{ m}^3 = 0.033 \text{ cm}^3

  4. The exact check. Rebuilding the rod dimension by dimension gives a new radius r(1σε)r(1 - \sigma\varepsilon) and a new length L(1+ε)L(1+\varepsilon), and multiplying those out gives ΔV=3.295×108\Delta V = 3.295 \times 10^{-8} m3^3 — the same to three figures, differing from the linear answer by 0.12%.

Final Answer: F=1.57×104F = 1.57 \times 10^{4} N, ΔVV=4.2×104\frac{\Delta V}{V} = 4.2 \times 10^{-4}, ΔV=3.30×108\Delta V = 3.30 \times 10^{-8} m3^3 (0.033 cm3^3).

Takeaway: The volume went UP. A stretched metal rod gains volume, because σ\sigma is less than 0.5. About 1.6 tonnes of force changes that rod's volume by three hundredths of a cubic centimetre.

Example 4: The incompressible material

A rubber cord is stretched. Assuming rubber has σ=0.5\sigma = 0.5 exactly, show that its volume does not change, and find what its diameter does when its length is increased by 20%.

Solution:

  1. The volume. Straight from the formula, ΔVV=(12σ)ΔLL=(12×0.5)ΔLL=0×ΔLL=0\frac{\Delta V}{V} = (1 - 2\sigma)\frac{\Delta L}{L} = (1 - 2 \times 0.5)\frac{\Delta L}{L} = 0 \times \frac{\Delta L}{L} = 0 whatever the strain is. The lengthening and the thinning cancel exactly.

  2. The diameter, using the linear formula. With ΔLL=0.20\frac{\Delta L}{L} = 0.20, Δdd=0.5×0.20=0.10\frac{\Delta d}{d} = -0.5 \times 0.20 = -0.10 so the diameter falls by 10%.

  3. Being honest about step 2. A strain of 20% is far outside the small-strain regime. Exactly conserving the volume requires d2Ld^{2}L to be constant, so dd=11.20=0.913\frac{d^{\,\prime}}{d} = \frac{1}{\sqrt{1.20}} = 0.913 — a fall of 8.7%, not 10%. The linear estimate is 15% out.

Final Answer: The volume is unchanged. The diameter falls by about 10% on the linear estimate, and by 8.7% on the exact constant-volume calculation.

Takeaway: σ=0.5\sigma = 0.5 is the definition of an incompressible material, and it is the only value for which stretching changes no volume. But at rubber-sized strains the linearised formulas are estimates, not answers — say so when you use them.

Example 5: From YY and σ\sigma to BB and GG

For steel, Y=2.0×1011Y = 2.0 \times 10^{11} Pa and σ=0.29\sigma = 0.29. Find the bulk modulus and the shear modulus.

Solution:

  1. Bulk modulus, from Y=3B(12σ)Y = 3B(1-2\sigma): B=Y3(12σ)=2.0×10113(10.58)=2.0×10113×0.42=2.0×10111.26B = \frac{Y}{3(1 - 2\sigma)} = \frac{2.0 \times 10^{11}}{3(1 - 0.58)} = \frac{2.0 \times 10^{11}}{3 \times 0.42} = \frac{2.0 \times 10^{11}}{1.26} B=1.587×1011 PaB = 1.587 \times 10^{11} \text{ Pa}

  2. Shear modulus, from Y=2G(1+σ)Y = 2G(1+\sigma): G=Y2(1+σ)=2.0×10112×1.29=2.0×10112.58=7.752×1010 PaG = \frac{Y}{2(1 + \sigma)} = \frac{2.0 \times 10^{11}}{2 \times 1.29} = \frac{2.0 \times 10^{11}}{2.58} = 7.752 \times 10^{10} \text{ Pa}

  3. Cross-check against the third relation. With these values, 3G+1B=37.752×1010+11.587×1011=4.500×1011=92.0×1011=9Y\frac{3}{G} + \frac{1}{B} = \frac{3}{7.752 \times 10^{10}} + \frac{1}{1.587 \times 10^{11}} = 4.500 \times 10^{-11} = \frac{9}{2.0 \times 10^{11}} = \frac{9}{Y} It closes exactly, as it must.

Final Answer: B=1.59×1011B = 1.59 \times 10^{11} Pa and G=7.75×1010G = 7.75 \times 10^{10} Pa.

Takeaway: The relations are self-consistent, so the third one is always a free check. Compute BB and GG from the first two, then verify with 9Y=3G+1B\frac{9}{Y} = \frac{3}{G} + \frac{1}{B}. If it does not close, you made an arithmetic slip. Note also that the tabulated values for real steel are B=1.6×1011B = 1.6 \times 10^{11} Pa and G=0.84×1011G = 0.84 \times 10^{11} Pa — close, but not identical, exactly as the honesty block warned.

Example 6: From GG and BB to YY and σ\sigma

A metal has G=0.84×1011G = 0.84 \times 10^{11} Pa and B=1.60×1011B = 1.60 \times 10^{11} Pa. Find YY and σ\sigma.

Solution:

  1. Poisson's ratio, straight from the elimination formula: σ=3B2G2(3B+G)\sigma = \frac{3B - 2G}{2(3B + G)} Compute the pieces: 3B=4.80×10113B = 4.80 \times 10^{11} and 2G=1.68×10112G = 1.68 \times 10^{11}, so the numerator is 3.12×10113.12 \times 10^{11}. The denominator is 2(4.80+0.84)×1011=1.128×10122(4.80 + 0.84) \times 10^{11} = 1.128 \times 10^{12}. σ=3.12×10111.128×1012=0.2766\sigma = \frac{3.12 \times 10^{11}}{1.128 \times 10^{12}} = 0.2766

  2. Young's modulus, from the reciprocal relation: 9Y=3G+1B=30.84×1011+11.60×1011\frac{9}{Y} = \frac{3}{G} + \frac{1}{B} = \frac{3}{0.84 \times 10^{11}} + \frac{1}{1.60 \times 10^{11}} 9Y=3.571×1011+0.625×1011=4.196×1011\frac{9}{Y} = 3.571 \times 10^{-11} + 0.625 \times 10^{-11} = 4.196 \times 10^{-11} Y=94.196×1011=2.145×1011 PaY = \frac{9}{4.196 \times 10^{-11}} = 2.145 \times 10^{11} \text{ Pa}

  3. Check both against the originals. 2G(1+σ)=2×0.84×1011×1.2766=2.145×10112G(1+\sigma) = 2 \times 0.84 \times 10^{11} \times 1.2766 = 2.145 \times 10^{11}. Agrees.

Final Answer: Y=2.14×1011Y = 2.14 \times 10^{11} Pa and σ=0.277\sigma = 0.277.

Takeaway: This is real steel's GG and BB, and the predicted YY comes out 7% above the measured 2.0×10112.0 \times 10^{11} Pa. That is the honest size of the disagreement between an ideal isotropic relation and a real polycrystalline metal — not an error in your working.

Example 7: Aluminium, three ways

For aluminium, G=2.5×1010G = 2.5 \times 10^{10} Pa and B=7.2×1010B = 7.2 \times 10^{10} Pa. Find YY and σ\sigma, and compare with the tabulated Y=7.0×1010Y = 7.0 \times 10^{10} Pa.

Solution:

  1. Young's modulus. 9Y=32.5×1010+17.2×1010=1.200×1010+0.1389×1010=1.3389×1010\frac{9}{Y} = \frac{3}{2.5 \times 10^{10}} + \frac{1}{7.2 \times 10^{10}} = 1.200 \times 10^{-10} + 0.1389 \times 10^{-10} = 1.3389 \times 10^{-10} Y=91.3389×1010=6.722×1010 PaY = \frac{9}{1.3389 \times 10^{-10}} = 6.722 \times 10^{10} \text{ Pa}

  2. Poisson's ratio. With 3B=2.16×10113B = 2.16 \times 10^{11} and 2G=5.0×10102G = 5.0 \times 10^{10}, σ=2.16×10115.0×10102(2.16×1011+2.5×1010)=1.66×10114.82×1011=0.344\sigma = \frac{2.16 \times 10^{11} - 5.0 \times 10^{10}}{2\,(2.16 \times 10^{11} + 2.5 \times 10^{10})} = \frac{1.66 \times 10^{11}}{4.82 \times 10^{11}} = 0.344

  3. Compare with the table. Predicted Y=6.72×1010Y = 6.72 \times 10^{10} Pa against a tabulated 7.0×10107.0 \times 10^{10} Pa — low by 4.0%. Predicted σ=0.344\sigma = 0.344 against a handbook 0.33 — high by about 4%.

Final Answer: Y=6.72×1010Y = 6.72 \times 10^{10} Pa and σ=0.344\sigma = 0.344, both within about 4% of the tabulated values.

Takeaway: Four per cent is a good result, not a bad one. Aluminium is one of the more nearly isotropic common metals, which is exactly why the relations do better here than they do for iron or glass.

Example 8: The material with σ=0.25\sigma = 0.25

A hypothetical solid has σ=0.25\sigma = 0.25 exactly. Express GG and BB as multiples of YY, and find GB\frac{G}{B}.

Solution:

  1. Shear modulus. G=Y2(1+0.25)=Y2.5=0.40YG = \frac{Y}{2(1 + 0.25)} = \frac{Y}{2.5} = 0.40\,Y

  2. Bulk modulus. B=Y3(10.50)=Y1.5=0.667YB = \frac{Y}{3(1 - 0.50)} = \frac{Y}{1.5} = 0.667\,Y

  3. Their ratio. GB=0.400.667=0.60\frac{G}{B} = \frac{0.40}{0.667} = 0.60

  4. Check with the elimination formula. Put G=0.6BG = 0.6B into σ=3B2G2(3B+G)\sigma = \frac{3B - 2G}{2(3B+G)}: numerator =3B1.2B=1.8B= 3B - 1.2B = 1.8B, denominator =2(3B+0.6B)=7.2B= 2(3B + 0.6B) = 7.2B, so σ=0.25\sigma = 0.25. Consistent.

Final Answer: G=0.40YG = 0.40Y, B=23YB = \frac{2}{3}Y, and GB=0.60\frac{G}{B} = 0.60.

Takeaway: σ=0.25\sigma = 0.25 is the classic examination value because every ratio comes out in round numbers. If a question gives you σ=0.25\sigma = 0.25, expect G=0.4YG = 0.4Y and B=2Y3B = \frac{2Y}{3} and save yourself the algebra.

Example 9: Why σ\sigma cannot exceed 0.5

Show, using the relations, that no isotropic material can have σ>0.5\sigma > 0.5 or σ<1\sigma < -1. What happens to BB and GG at the two limits?

Solution:

  1. The upper bound. From Y=3B(12σ)Y = 3B(1 - 2\sigma), rearranged as B=Y3(12σ)B = \frac{Y}{3(1-2\sigma)}. Both YY and BB must be positive for a stable material. If σ>0.5\sigma > 0.5 then (12σ)<0(1-2\sigma) < 0 and BB would be negative — meaning the body would expand when you compressed it, releasing energy indefinitely. That is impossible, so σ0.5\sigma \leq 0.5.

  2. At the limit itself. As σ0.5\sigma \to 0.5, (12σ)0(1-2\sigma) \to 0 and BB \to \infty. Infinite bulk modulus means zero compressibility: the material cannot be squeezed at all. This is exactly the incompressible case.

  3. The lower bound. From G=Y2(1+σ)G = \frac{Y}{2(1+\sigma)}. If σ<1\sigma < -1 then (1+σ)<0(1+\sigma) < 0 and GG would be negative, so σ1\sigma \geq -1.

  4. At that limit. As σ1\sigma \to -1, GG \to \infty: the material would resist any shearing absolutely.

Final Answer: 1σ0.5-1 \leq \sigma \leq 0.5. At σ=0.5\sigma = 0.5 the bulk modulus becomes infinite; at σ=1\sigma = -1 the shear modulus becomes infinite.

Takeaway: The bounds are not measured, they are forced. They come from nothing more than the demand that BB and GG be positive, which in turn is the demand that a material not be a free source of energy.

Example 10: Three routes, three answers

For steel take Y=200Y = 200 GPa, G=84G = 84 GPa and B=160B = 160 GPa, all from measurement. Compute σ\sigma three ways and comment.

Solution:

  1. From YY and GG: σ=Y2G1=2001681=1.1901=0.190\sigma = \frac{Y}{2G} - 1 = \frac{200}{168} - 1 = 1.190 - 1 = 0.190

  2. From YY and BB: σ=12(1Y3B)=12(1200480)=12(10.4167)=0.292\sigma = \frac{1}{2}\left(1 - \frac{Y}{3B}\right) = \frac{1}{2}\left(1 - \frac{200}{480}\right) = \frac{1}{2}(1 - 0.4167) = 0.292

  3. From GG and BB: σ=3B2G2(3B+G)=4801682(480+84)=3121128=0.277\sigma = \frac{3B - 2G}{2(3B+G)} = \frac{480 - 168}{2(480 + 84)} = \frac{312}{1128} = 0.277

  4. Comment. The three answers are 0.190, 0.292 and 0.277 — a spread of about 0.10, or roughly 40% of the middle value. The accepted handbook figure for structural steel is about 0.29, so the Y,BY,B and G,BG,B routes are good and the Y,GY,G route is poor. The culprit is the rounded G=84G = 84 GPa; the value for common structural steel is nearer 79 GPa, and using that gives σ=0.266\sigma = 0.266.

Final Answer: 0.190, 0.292 and 0.277 respectively. The true value is about 0.29.

Takeaway: A ten per cent error in one modulus becomes a much larger error in σ\sigma, because σ\sigma from YY and GG is a small difference between two numbers near 1. Never quote a Poisson's ratio obtained this way to more than two figures.

Example 11: Percentage volume change

A metal wire with σ=0.30\sigma = 0.30 is stretched by 0.20% of its length. By what percentage does its volume change, and in which direction?

Solution:

  1. Substitute directly. ΔVV=(12σ)ΔLL=(10.60)×2.0×103=0.40×2.0×103\frac{\Delta V}{V} = (1 - 2\sigma)\frac{\Delta L}{L} = (1 - 0.60) \times 2.0 \times 10^{-3} = 0.40 \times 2.0 \times 10^{-3} ΔVV=8.0×104=0.080%\frac{\Delta V}{V} = 8.0 \times 10^{-4} = 0.080\%

  2. The direction. (12σ)(1-2\sigma) is positive, so the volume increases.

  3. Exact check. Multiplying out the actual deformed dimensions gives 7.98×1047.98 \times 10^{-4} — the linear answer is high by 0.26%, which is negligible at this strain.

Final Answer: The volume increases by 0.080%.

Takeaway: A 0.20% stretch produces only a 0.080% volume gain, because most of the lengthening is paid for by the sideways shrinking. The factor (12σ)=0.40(1-2\sigma) = 0.40 is exactly the fraction that survives.

Example 12: From volume change back to Poisson's ratio

A rod is stretched so that its length increases by 0.50%. Its volume is found to increase by 0.10%. Find Poisson's ratio for the material and identify a likely candidate from the reference list.

Solution:

  1. Write the relation and solve for σ\sigma. ΔVV=(12σ)ΔLL    12σ=ΔV/VΔL/L\frac{\Delta V}{V} = (1 - 2\sigma)\frac{\Delta L}{L} \;\Longrightarrow\; 1 - 2\sigma = \frac{\Delta V / V}{\Delta L / L}

  2. Substitute the two percentages — note that both are fractions, so the units cancel and you may divide the percentages directly: 12σ=0.10%0.50%=0.201 - 2\sigma = \frac{0.10\%}{0.50\%} = 0.20

  3. Rearrange. 2σ=10.20=0.80    σ=0.402\sigma = 1 - 0.20 = 0.80 \;\Longrightarrow\; \sigma = 0.40

  4. Identify it. From the reference list, σ=0.40\sigma = 0.40 sits between titanium (0.36) and gold (0.42) — a soft, dense metal. It is far too high for steel or glass.

Final Answer: σ=0.40\sigma = 0.40.

Takeaway: The ratio of the two percentages is (12σ)(1 - 2\sigma) directly. You do not need the length, the diameter, the force or the modulus — this is a pure-ratio question, and recognising that turns a page of work into two lines.