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Heating at constant pressure. T-v curves for a range of pressures.

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Heating at constant pressure
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Page 1: Heating at constant pressure. T-v curves for a range of pressures.

Heating at constant pressure

Page 2: Heating at constant pressure. T-v curves for a range of pressures.
Page 3: Heating at constant pressure. T-v curves for a range of pressures.
Page 4: Heating at constant pressure. T-v curves for a range of pressures.
Page 5: Heating at constant pressure. T-v curves for a range of pressures.
Page 6: Heating at constant pressure. T-v curves for a range of pressures.

T-v curves for a rangeof pressures

Page 7: Heating at constant pressure. T-v curves for a range of pressures.

T-v phase diagram

Page 8: Heating at constant pressure. T-v curves for a range of pressures.

P-v diagram

Page 9: Heating at constant pressure. T-v curves for a range of pressures.

P-T diagram

vapor

liquid

critical point

coex

iste

nce

curv

e

Page 10: Heating at constant pressure. T-v curves for a range of pressures.

compressed liquid ≈ saturated liquidat the same

temperature

Steam, water, water vapor, refrigerantsUse property tables

Air, helium gas, etc.Use ideal gas law and specific

heats.

Enthalpy

H = U + PV h = u + Pv

Page 11: Heating at constant pressure. T-v curves for a range of pressures.

ExampleWe have 30 l of water in a piston. The initial temperature is 40°C and the pressure is kept constant at 500 kPa. We now heat the water (still at constant pressure) until all water is in the vapor phase. We keep heating the vapor further until the volume is has expanded to 30 m3.

1) What is the temperature of the water vapor at the point where everything has just turned into vapor?2) What is the temperature when the water vapor has expanded to 30 m3?3) What is the change in enthalpy between the initial and final states ?

Initially, the water is in the compressed liquid state; 500 kPa is well above the saturated vapor pressure at 40°C. By adding heat we keep increasing the temperature until we hit the coexistence curve. At that point T = Tsat(500 kPa) = 152 °C. Adding more heat leads to gradual evaporation of the liquid (at constant temperature.)

The final temperature we get from the superheated vapor table. We know P= 500 kPa. Looking in that section of the table we see that v≈ 1 m3/kg when we reach T = 800°C

V

Enthalpy change:We approximate the properties of the compressed liquid with those of saturated liquid at 40°C h1 = hf(40°C) = 167.5 kJ/kg

When everything has just turned into vapor we have h2 = hg(500 kPa) = 2748.1 kJ/kg

And at P= 500 kPa, T= 800°C we find h3=4158.4 kJ/kg.

To get the total enthalpy change we multiply the change in the specific enthalpy by the mass of the fluid, which we find from the initial conditions. M = V/v.

Page 12: Heating at constant pressure. T-v curves for a range of pressures.

Use of tablesSaturated

T P, vf, vg, uf, ug, etc.

P T, vf, vg, uf, ug, etc.

but alsouf T, P, vf, vg, uf, ug, etc.

Superheated vaporyou need to know two properties(T,P) or (T,u) or (P,v) etc.

Page 13: Heating at constant pressure. T-v curves for a range of pressures.

Steady flow work

The first Tds-equation:

Tds = du + Pdv

Enthalpy:

h = u + Pv dh =du + Pdv +vdP

The second Tds-equation:

Tds = dh - vdP

Page 14: Heating at constant pressure. T-v curves for a range of pressures.

Reversible steady flowand compression work

Steady flow:

dh = δqin – δwout

Reversible: δqin = Tds

dh = Tds – δwout

But also:

dh = Tds + vdP

So:

δwout = -vdP

wout = -∫vdP wcomp = ∫vdP

Page 15: Heating at constant pressure. T-v curves for a range of pressures.

Why does this matter?

wout = -∫vdP compressing a gas requires much

more work than compressing a liquid !

In a Rankine (steam) cycle we compress liquid and expand vapor.

For liquids, v ~ constantwcompression = vΔP

Page 16: Heating at constant pressure. T-v curves for a range of pressures.

Steam qualityThe purpose of a turbine is to convert enthalpy into work. From

that point of view, steam with a large enthalpy is good.

On expansion, the pressure and temperature of the steam drop, and some may condense. The specific enthalpy of the liquid is much smaller than the specific enthalpy of the vapor. The (mass) fraction of the vapor is called the “quality” of the steam, x. The remaining fraction, (1-x) is liquid.

To calculate any property of a mixture of liquid and vapor, e.g. the specific enthalpy

h = xhg + (1 – x)hf.

The subscripts g and f stand for the gas/vapor and fluid/liquid phases.

Page 17: Heating at constant pressure. T-v curves for a range of pressures.

Figures come mainly from

Thermodynamics

by Y.A Cengel and M.A. Boles


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