Pump up a bicycle tyre quickly, twenty strokes without a pause, and feel the lower end of the pump. It is warm, sometimes hot. No flame came near it, and friction at the piston is small. Now let air out of the tyre valve onto your hand. It feels cold. Squeezing air warms it, and letting it spread cools it.
No heat in, no heat out
In an adiabatic process no heat crosses the boundary: \(Q = 0\). There are two ways to arrange this. The gas can be wrapped in good insulation, as in a vacuum flask. Or the change can be so fast that heat has no time to flow, as in a quick stroke of a pump. This lesson uses \(R = 8.31\,\text{J/(mol K)}\) and \(\gamma = C_p/C_v = 1.4\) for air.
With \(Q = 0\), the first law says \(W = -\Delta U\). A gas that expands adiabatically does positive work, and it can pay only from its own internal energy. So \(U\) falls and the gas cools. A gas compressed adiabatically has work done on it, and nowhere to lose the energy. So \(U\) rises and the gas warms. That is the pump and the valve.
For a quasi-static adiabatic change of an ideal gas, the pressure and volume follow a definite law. The derivation below combines the first law with the ideal gas equation.
\[ nC_v\,dT = -p\,dV \]
Why. the first law with \(dQ = 0\), using \(dU = nC_v\,dT\), which holds in every process of an ideal gas.
\[ p\,dV + V\,dp = nR\,dT \]
Why. the change in both sides of \(pV = nRT\) over a small step.
\[ C_v\,(p\,dV + V\,dp) = -R\,p\,dV \]
Why. multiply step 2 by \(C_v\) and replace \(nC_v\,dT\) using step 1.
\[ C_v\,V\,dp + (C_v + R)\,p\,dV = 0 \]
Why. collect the \(p\,dV\) terms on one side.
\[ \dfrac{dp}{p} + \gamma\,\dfrac{dV}{V} = 0 \]
Why. \(C_v + R = C_p\) by Mayer's relation; divide by \(C_v\,pV\) and write \(\gamma = C_p/C_v\).
\[ pV^\gamma = \text{constant} \]
Read it. integrate to get \(\ln p + \gamma\ln V = \text{constant}\), then take exponentials.
Two more forms follow by putting \(p = nRT/V\) or \(V = nRT/p\) into \(pV^\gamma\). They are \(TV^{\gamma - 1} = \text{constant}\) and \(p^{1-\gamma}T^\gamma = \text{constant}\). The work done also has a neat form. Since \(W = -\Delta U = nC_v(T_1 - T_2)\) and \(C_v = R/(\gamma - 1)\), the work is \(nR(T_1 - T_2)/(\gamma - 1)\). With \(pV = nRT\) this is \((p_1V_1 - p_2V_2)/(\gamma - 1)\).
One mole of air at \(300\,\text{K}\) is compressed adiabatically to \(1/32\) of its volume. Find its final temperature, the factor by which its pressure rises, and the work done on it.
\(TV^{\gamma - 1}\) is constant, so \(T_2 = 300 \times 32^{0.4} = 300 \times 4 = 1200\,\text{K}\).
\(pV^\gamma\) is constant, so \(p_2/p_1 = 32^{1.4} = 128\).
The work done on the gas is \(\Delta U\) \(= nC_v\,\Delta T\) \(= \tfrac52 \times 8.31 \times 900\) \(= 18\,700\,\text{J}\), since \(Q = 0\).
Helium (\(\gamma = 5/3\)) at \(900\,\text{K}\) expands adiabatically to \(8\) times its volume. What is its final temperature, in kelvin?
The adiabat is steeper
The curve \(pV^\gamma = \text{constant}\) is an adiabat. Through any state it falls more steeply than the isotherm. Take the change of \(pV = \text{constant}\) over a small step: \(p\,dV + V\,dp = 0\), so the isotherm's slope is \(dp/dV = -p/V\). The adiabatic law, \(dp/p + \gamma\,dV/V = 0\), gives a slope \(-\gamma p/V\). As \(\gamma > 1\), the adiabat is \(\gamma\) times as steep.
The physics is simple. In an isothermal expansion the pressure falls only because the volume grows. In an adiabatic expansion the gas also cools, and a cooler gas pushes less. Both effects lower the pressure, so it falls faster.
Play the chips of Fig 5.1. The isothermal gas takes in \(1728\,\text{J}\) of heat and turns it all into work. The adiabatic gas takes in nothing, so its \(1509\,\text{J}\) of work comes from its internal energy. Its temperature falls to \(300 \times 0.5^{0.4} = 227\,\text{K}\), and its molecules visibly slow down. In the both chip, the band between the two curves is the extra \(219\,\text{J}\) that the isothermal gas does.
The same two slopes set how hard a gas is to squeeze. The bulk modulus is \(B = -V\,dp/dV\). The isotherm gives \(B = p\), and the adiabat gives \(B = \gamma p\). For air at \(10^5\,\text{Pa}\) these are \(1.0 \times 10^5\,\text{Pa}\) and \(1.4 \times 10^5\,\text{Pa}\). A sound wave squeezes and releases the air so fast that heat cannot flow, so sound uses the adiabatic value. The unit on waves meets this as Laplace's correction.
For a monatomic ideal gas, what is the ratio of the slope of the adiabat to the slope of the isotherm through the same state?
Cylinder X has thin copper walls and stands in a large water bath. Cylinder Y has thick insulated walls. In each, a piston compresses the gas. Which statement is right?
A molecule meets a moving piston
The first law says a compressed gas warms. Kinetic theory shows how. Think of one molecule bouncing off a piston, like a cricket ball off a moving bat.
A molecule moving at \(400\,\text{m/s}\) hits a piston head-on. The piston is moving towards it at \(100\,\text{m/s}\). With what speed does the molecule bounce back?
In the frame of the piston the bounce is elastic. The molecule arrives at \(400 + 100 = 500\,\text{m/s}\) and leaves at \(500\,\text{m/s}\). Back in the frame of the cylinder, add the piston's velocity: the molecule leaves at \(600\,\text{m/s}\). Each hit on a piston moving in adds twice the piston's speed. A piston moving out takes it away: the molecule returns at only \(200\,\text{m/s}\). The lower half of the figure shows a whole gas. Pushed in, its molecules speed up and its temperature rises; drawn out, they slow down.
Now the pump. A quick stroke squeezes the air from \(1\,\text{atm}\) to about \(3\,\text{atm}\) too fast for heat to escape. By \(p^{1-\gamma}T^\gamma = \text{constant}\), air starting at \(300\,\text{K}\) reaches \(T = 300 \times 3^{0.4/1.4} = 411\,\text{K}\). Between strokes this hot air gives its heat to the barrel. The barrel is far heavier than the air, so it warms only by a few degrees per stroke, but twenty strokes add up.
The valve works the other way. Air at \(3\,\text{atm}\) that rushes out to \(1\,\text{atm}\) expands adiabatically and cools. Ideally it would reach \(300 \times (1/3)^{0.4/1.4} = 219\,\text{K}\). In practice it mixes with room air at once, but it still feels cold on the hand. A punctured tyre hisses cold air for the same reason.
A petrol engine lights its fuel with a spark. A diesel engine, in every truck, tractor and railway locomotive of India, has no spark plug. It squeezes air adiabatically to one sixteenth of its volume. Air entering at \(300\,\text{K}\) reaches \(300 \times 16^{0.4} = 909\,\text{K}\), about \(636\,\text{°C}\), at \(16^{1.4} = 48.5\) times its starting pressure. Diesel fuel sprayed into this air catches fire by itself, since it ignites above about \(500\,\text{K}\).
A gas expands isothermally at \(300\,\text{K}\). It is then compressed adiabatically back to its original volume. How does its final temperature compare with \(300\,\text{K}\)?
In 1893 the German engineer Rudolf Diesel patented an engine that would light its fuel by compression alone. He had read that the best engines waste as little heat as possible, and he wanted the air to heat itself. His first test engine blew apart, nearly killing him. By 1897 a working engine turned about a quarter of its fuel's heat into work, twice as much as the steam engines of his day.
Why the mountains keep their snow
In June the plains of north India bake at \(40\,\text{°C}\), yet the high Himalaya stays white. The air is heated from below, by the ground. A warm parcel of air rises, and as it rises the pressure around it falls, as the barometric formula showed. So the parcel expands. Air is a poor conductor and the parcel is large, so almost no heat flows in: the expansion is adiabatic. The parcel cools as it climbs. This part uses \(g = 9.8\,\text{m/s}^2\), as the atmosphere needs, and \(M = 0.029\,\text{kg/mol}\) for air.
\[ dQ = nC_v\,dT + p\,dV = 0 \]
Why. the first law for a small adiabatic step of the parcel.
\[ p\,dV = nR\,dT - V\,dp \]
Why. the change of \(pV = nRT\) is \(p\,dV + V\,dp = nR\,dT\).
\[ nC_p\,dT = V\,dp \]
Why. put step 2 into step 1 and use \(C_v + R = C_p\).
\[ V\,dp = -nMg\,dh \]
Why. the pressure falls by the weight of the air, \(dp = -\rho g\,dh\), and the parcel's density is \(\rho = nM/V\).
\[ \dfrac{dT}{dh} = -\dfrac{Mg}{C_p} \]
Read it. equate steps 3 and 4 and divide by \(nC_p\,dh\).
For dry air \(C_p = \tfrac72 R = 29.1\,\text{J/(mol K)}\). So the adiabatic lapse rate is \(Mg/C_p\) \(= 0.029 \times 9.8/29.1\) \(= 0.0098\,\text{K/m}\), about \(9.8\,\text{K}\) per kilometre. Dry air that leaves the plains at \(35\,\text{°C}\) would reach \(0\,\text{°C}\) after \(35/9.8 = 3.6\,\text{km}\).
The real atmosphere cools more slowly, about \(6.5\,\text{K}\) per kilometre on average. Rising air carries water vapour. When it cools enough, the vapour condenses into cloud and gives back its latent heat, which warms the parcel. At \(6.5\,\text{K}\) per kilometre, air at \(35\,\text{°C}\) reaches freezing near \(5.4\,\text{km}\). That is about where the summer snow line lies on the Himalaya.
A parcel of dry air at \(30\,\text{°C}\) rises \(2\,\text{km}\) without exchanging heat. Take the lapse rate as \(9.8\,\text{K/km}\). What is its temperature now, in °C?
- Thinking an adiabatic gas keeps its temperature because no heat flows.No heat flows, but work is done. \(W = -\Delta U\), so expansion cools the gas and compression warms it.
- Using \(TV^\gamma\) or \(pV^{\gamma - 1}\) by mistake.The three forms are \(pV^\gamma\), \(TV^{\gamma - 1}\) and \(p^{1-\gamma}T^\gamma\). Derive the one you need from \(pV^\gamma\) and \(pV = nRT\).
- Drawing the adiabat flatter than the isotherm.The adiabat's slope is \(\gamma\) times the isotherm's, and \(\gamma > 1\). The adiabat is always the steeper curve.