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fundamentals of engineering supplied-reference handbook - Ventech!

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SECOND LAW OF THERMODYNAMICS<br />

Thermal Energy Reservoirs<br />

∆Sreservoir = Q/Treservoir , where<br />

Q is measured with respect to the reservoir.<br />

Kelvin-Planck Statement <strong>of</strong> Second Law<br />

No heat engine can operate in a cycle while transferring heat<br />

with a single heat reservoir.<br />

COROLLARY to Kelvin-Planck: No heat engine can have a<br />

higher efficiency than a Carnot cycle operating between the<br />

same reservoirs.<br />

Clausius' Statement <strong>of</strong> Second Law<br />

No refrigeration or heat pump cycle can operate without a<br />

net work input.<br />

COROLLARY: No refrigerator or heat pump can have a<br />

higher COP than a Carnot cycle refrigerator or heat pump.<br />

VAPOR-LIQUID MIXTURES<br />

Henry's Law at Constant Temperature<br />

At equilibrium, the partial pressure <strong>of</strong> a gas is proportional<br />

to its concentration in a liquid. Henry's Law is valid for low<br />

concentrations; i.e., x ≈ 0.<br />

pi = pyi = hxi, where<br />

h = Henry's Law constant,<br />

pi = partial pressure <strong>of</strong> a gas in contact with a liquid,<br />

xi = mol fraction <strong>of</strong> the gas in the liquid,<br />

yi = mol fraction <strong>of</strong> the gas in the vapor, and<br />

p = total pressure.<br />

Raoult's Law for Vapor-Liquid Equilibrium<br />

Valid for concentrations near 1; i.e., xi ≈ 1.<br />

pi = xi pi * , where<br />

pi = partial pressure <strong>of</strong> component i,<br />

xi = mol fraction <strong>of</strong> component i in the liquid, and<br />

pi * = vapor pressure <strong>of</strong> pure component i at the<br />

temperature <strong>of</strong> the mixture.<br />

ENTROPY<br />

ds = (1/T) δQrev<br />

( )<br />

2<br />

2 1 1 1/ − = ∫ δ rev<br />

s s T Q<br />

Inequality <strong>of</strong> Clausius<br />

∫ (1/ T ) δQ<br />

≤ 0<br />

2<br />

1<br />

∫<br />

( )<br />

rev<br />

1/T δQ≤ s −s<br />

2 1<br />

Isothermal, Reversible Process<br />

∆s = s2 – s1 = Q/T<br />

60<br />

Isentropic Process<br />

∆s = 0; ds = 0<br />

A reversible adiabatic process is isentropic.<br />

Adiabatic Process<br />

δQ = 0; ∆s ≥ 0<br />

Increase <strong>of</strong> Entropy Principle<br />

∆stotal<br />

= ∆ssystem<br />

+ ∆ssurroundings<br />

≥ 0<br />

∆s�<br />

total = ∑m�outsout − ∑m�insin<br />

− ∑ Q�<br />

T ≥<br />

THERMODYNAMICS (continued)<br />

( )<br />

external<br />

external<br />

Temperature-Entropy (T-s) Diagram<br />

Q rev<br />

= ∫<br />

2<br />

T ds<br />

1<br />

Entropy Change for Solids and Liquids<br />

ds = c (dT/T)<br />

s2 – s1 = ∫ c (dT/T) = cmeanln (T2 /T1),<br />

where c equals the heat capacity <strong>of</strong> the solid or liquid.<br />

Irreversibility<br />

I = wrev – wactual<br />

EXERGY<br />

Exergy is the portion <strong>of</strong> total energy available to do work.<br />

Closed-System Availability<br />

(no chemical reactions)<br />

φ = (u – uo) – To (s – so) + po (v – vo)<br />

where the subscript "o" designates environmental conditions<br />

wreversible = φ1 – φ2<br />

Open-System Availability<br />

ψ = (h – ho) – To (s – so) + V 2 /2 + gz<br />

wreversible = ψ1 – ψ2<br />

Gibbs Free Energy, ∆G<br />

Energy released or absorbed in a reaction occurring<br />

reversibly at constant pressure and temperature.<br />

Helmholtz Free Energy, ∆A<br />

Energy released or absorbed in a reaction occurring<br />

reversibly at constant volume and temperature.<br />

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