First Law of Thermodyamics U = Q + W. We can rewrite this by introducing two physical. Enthalpy, H, is the quantity U + pv, as this

Similar documents
Thermodynamics Review [?] Entropy & thermodynamic potentials Hydrostatic equilibrium & buoyancy Stability [dry & moist adiabatic]

Buoyancy and Coriolis forces

Thermodynamic Energy Equation

Measuring State Parameters of the Atmosphere

ATMO 551a Moist Adiabat Fall Change in internal energy: ΔU

Radiative equilibrium Some thermodynamics review Radiative-convective equilibrium. Goal: Develop a 1D description of the [tropical] atmosphere

NENG 301 Week 8 Unary Heterogeneous Systems (DeHoff, Chap. 7, Chap )

Entropy in Macroscopic Systems

Exam 1 (Chaps. 1-6 of the notes)

Measuring State Parameters of the Atmosphere

2 Equations of Motion

Applied Thermodynamics for Marine Systems Prof. P. K. Das Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Thermodynamic Third class Dr. Arkan J. Hadi

Chapter 3 - First Law of Thermodynamics

Chapter 6 Thermodynamic Properties of Fluids

Irreversible Processes

Chapter 3. Property Relations The essence of macroscopic thermodynamics Dependence of U, H, S, G, and F on T, P, V, etc.

ATMOS 5130 Lecture 9. Enthalpy Conservation Property The Second Law and Its Consequences Entropy

Chemistry. Lecture 10 Maxwell Relations. NC State University

S A 0.6. Units of J/mol K S U /N

GEF2200 Atmosfærefysikk 2012

...Thermodynamics. Entropy: The state function for the Second Law. Entropy ds = d Q. Central Equation du = TdS PdV

Convection and buoyancy oscillation

Irreversible Processes

Temperature and Thermodynamics, Part II. Topics to be Covered

Thermodynamics and Phase Transitions in Minerals

The Second Law of Thermodynamics

4) It is a state function because enthalpy(h), entropy(s) and temperature (T) are state functions.

Thermodynamics. Basic concepts. Thermal equilibrium and temperature

Module 5 : Electrochemistry Lecture 21 : Review Of Thermodynamics

Today s Lecture: Atmosphere finish primitive equations, mostly thermodynamics

First Law of Thermodynamics

Enthalpy and Adiabatic Changes

MATTER TRANSPORT (CONTINUED)

df dz = dp dt Essentially, this is just a statement of the first law in one of the forms we derived earlier (expressed here in W m 3 ) dq p dt dp

Lecture 15. Available Work and Free Energy. Lecture 15, p 1

Introduction into thermodynamics

Chapter 3. Entropy, temperature, and the microcanonical partition function: how to calculate results with statistical mechanics.

The Second Law of Thermodynamics (Chapter 4)

ADIABATIC PROCESS Q = 0

Thermodynamics: A Brief Introduction. Thermodynamics: A Brief Introduction

References: Parcel Theory. Vertical Force Balance. ESCI Cloud Physics and Precipitation Processes Lesson 3 - Stability and Buoyancy Dr.

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name:

Minimum Bias Events at ATLAS

GEF2200 vår 2017 Løsningsforslag sett 1

Classical Thermodynamics. Dr. Massimo Mella School of Chemistry Cardiff University

4. All questions are NOT ofequal value. Marks available for each question are shown in the examination paper.

ESCI 341 Atmospheric Thermodynamics Lesson 12 The Energy Minimum Principle

Atmospheric Thermodynamics

Chapter 6. Using Entropy

Physics 607 Final Exam

Problem: Calculate the entropy change that results from mixing 54.0 g of water at 280 K with 27.0 g of water at 360 K in a vessel whose walls are

1 mol ideal gas, PV=RT, show the entropy can be written as! S = C v. lnt + RlnV + cons tant

The Thermodynamics of. The rst law ofthermodynamics relates the change in internal energy to the

dg = V dp - S dt (1.1) 2) There are two T ds equations that are useful in the analysis of thermodynamic systems. The first of these

Math 1270 Honors ODE I Fall, 2008 Class notes # 14. x 0 = F (x; y) y 0 = G (x; y) u 0 = au + bv = cu + dv

Radiative Transfer Chapter 3, Hartmann

The Tropical Atmosphere: Hurricane Incubator

Copyright 2008, University of Chicago, Department of Physics. Experiment I. RATIO OF SPECIFIC HEATS OF GASES; γ C p

Multivariable Calculus

Physics 408 Final Exam

Marginal Functions and Approximation

Chapter 2 Carnot Principle

39th International Physics Olympiad - Hanoi - Vietnam Theoretical Problem No. 3 / Solution. Solution

UNIVERSITY OF SOUTHAMPTON

Work - kinetic energy theorem for rotational motion *

MS212 Thermodynamics of Materials ( 소재열역학의이해 ) Lecture Note: Chapter 7

3. First Law of Thermodynamics and Energy Equation

General Concepts of Atmospheric Thermodynamic Atmospheric Thermodynamic Theory

Lecture 3: Convective Heat Transfer I

Thermodynamics of the Heat Engine

where (E) is the partition function of the uniform ensemble. Recalling that we have (E) = E (E) (E) i = ij x (E) j E = ij ln (E) E = k ij ~ S E = kt i

10, Physical Chemistry- III (Classical Thermodynamics, Non-Equilibrium Thermodynamics, Surface chemistry, Fast kinetics)

Thermodynamics of the Heat Engine

OCN 623: Thermodynamic Laws & Gibbs Free Energy. or how to predict chemical reactions without doing experiments

ATMO 551a Fall 08. Equivalent Potential Temperature

IV. Compressible flow of inviscid fluids

CHAPTER 7 ENTROPY. Copyright Hany A. Al-Ansary and S. I. Abdel-Khalik (2014) 1

WHY SHOULD WE CARE ABOUT THERMAL PHENOMENA? they can profoundly influence dynamic behavior. MECHANICS.

CHAPTER 3 LECTURE NOTES 3.1. The Carnot Cycle Consider the following reversible cyclic process involving one mole of an ideal gas:

Worksheet for Exploration 21.1: Engine Efficiency W Q H U

Quantities and Variables in Thermodynamics. Alexander Miles

Summarizing, Key Point: An irreversible process is either spontaneous (ΔS universe > 0) or does not occur (ΔS universe < 0)

Atmospheric Physics. August 10, 2017

Entropy A measure of molecular disorder

The Role of Water Vapor. atmosphere (we will ignore the solid phase here) Refer to the phase diagram in the web notes.

1. The vertical structure of the atmosphere. Temperature profile.

in order to insure that the Liouville equation for f(?; t) is still valid. These equations of motion will give rise to a distribution function f(?; t)

I.G Approach to Equilibrium and Thermodynamic Potentials

AAE COMBUSTION AND THERMOCHEMISTRY

General Physics I (aka PHYS 2013)

General Gibbs Minimization as an Approach to Equilibrium

Engineering Thermodynamics. Chapter 6. Entropy: a measure of Disorder 6.1 Introduction

8.21 The Physics of Energy Fall 2009

Introduction Statistical Thermodynamics. Monday, January 6, 14

Final Review Prof. WAN, Xin

S = S(f) S(i) dq rev /T. ds = dq rev /T

UNIVERSITY OF SOUTHAMPTON

Monday 7 October 2013, Class #15

Physics 172H Modern Mechanics

Transcription:

First Law of Thermodyamics U = Q + W where U is the increase in internal energy of the system, Q is the heat supplied to the system and W is the work done on the system. We can rewrite this by introducing two physical concepts, entropy and enthalpy. Entropy, S, is a measure of disorder in the system. Enthalpy, H, is the quantity U + pv, as this combination of terms frequently appears in thermodynamic equations. so we can rewrite the rst law in terms of entropy and enthalpy by considering conditions of constant pressure or constant volume: U = TS,pV H = TS +Vp For a simplyfying assumption we consider only reversible changes so that Q = TS;W = pv Specic Heats At constant volume:

which becomes c v =( dq dt ) c v =( du dt )! U = c vt for an ideal gas (pv = RT). Therefore, H = c v T + RT = T(c v + R) =c p T!H = c p T where c p is the specic heat at constant pressure. We can then solve for TS TS = H, Vp eliminating V yields TS = c p T, ( RT p )p Dividing by T yields a convenient form: S = c p ( T T ), R(p p ) and integrating over all the 's yields (A) S = c p (lnt),r(lnp)+s o! S = c p (ln(tp, ))+S o where R cp

For a diatomic gas, is approximately 2/7. Now let's consider an adiabatic process, one in which there is no heat transfer. This means Q = 0 which, by our denition means S =0. To fullll this condition means c p ( T T )=R(p p ) if the system goes from T to a nal temperature T f and from p to p o then when we integrate the lefthand side from T to T f and the righthand side from p to p o we get or c p (ln( T f T )) = R(ln(p o p )) T f = T ( p o p) The quantity T f is usually referred to as and is known as the potential temperature. For reference, p o is usually taken to be 1000 millibars. Parcels of Air and Lapse Rates We assume that a parcel of air is like our idealized cylinder. The parcel is in pressure equilibrium with respect to the environment but may have diering temperature and density. Of course, there is no such thing as a parcel as real air mixes fast.

For an adiabatic parcel, the potential temperature and entropy are constant as heigh changes so we can write: d dz ] parcel =[ds dz ] =0 parcel or from equation A c p T dz ], R dp parcel p dz ] =0 parcel or rearranging terms dz ]=RT dp c p p dz ] (B) Now we remember hydrostatic equilibrium to yield dp dz =,gp RT dz ]=,g c p or more conveniently, dz ]= g c p This species the rate of temperature decrease with height (z) that would be expected for an adiabatic parcel of air. So this is called the adiabatic

lapse rate. In its simplest form when applied to a mass of dry air its value is 9.8 K/km. The introduction of this concept now allows for us to physically dene a stability criterion. We consider a parcel of air with parameters T,p, and z which adiabatically rises to a height z. At this new height z 1 = z + z. The new temparature will be: or T 1 = T + dz ] parcel z T 1 = T, g c p z The environmetal temperature, at height z 1 will be dierent than T 1 put the parcel is assumed to be in pressure equilibrium so that p 1 = p + dp dz ] env z Using the ideal gas law p 1 parcel = ; env = p 1 RT parcel RT env stability occurs whenever parcel is greater than env ; the displaced parcel can't continue to rise and will fall back down, Instability occurs if the rising

parcel nds its density to be less than the density of the environment. Hence the concept of buoyancy now comes into play. The buoyancy force occurs because the eective mass is dierent at height z than it is at z 1 as we assume constant volume for the parcel of air (there are no pressure dierences to cause expansion or contraction). The mass dierence is V 1 ( e, pl ) where e refers to environment and pl refers to parcel. Now we apply newtons second law: F = mx Now the notation gets a little cumbersome but: Force= gv 1 ( e, pl )= pl V 1 d2 (z) dt 2 d 2 (z) = g[ e, 1]) = g[ T pl, 1] dt 2 pl T e now we use our previous expressions for T e and T pl and dene to get, a = dt ;,= dt dz parcel dz env d 2 (z) dt 2 = g[ (T,, az) (T,,z), 1)

or d 2 (z) dt 2 =, g T (, a,,)z This reduces to an equation of the form: where N 2 d 2 (z) dt 2 + N 2 (z)=0 = g T (, a,,) = g T ( dz + g c p ) where T in this case is environmental temperature. If N 2 > 0 then this is the equation of motion for a harmonic oscillator where N is the frequency (called buoyancy frequency). We can return to our previous equation: or =T( p o p ) ln =lnt, lnp dierentiating yields d = T, dp p now we diereniate both sidez by dz

1 d dz = 1 T remember that dp =,g dz so now since = R cp 1 d dz = 1 T dp dz, p dz dz + g p and the ideal gas law we get 1 d dz + dz = 1 T so that N 2 = g d dz as the stability criteria. g c p T