First Name Last Name CIRCLE YOUR LECTURE BELOW: Div. 1 10:30 am Div. 2 2:30 pm Div. 3 4:30 pm Prof. Gore Prof. Udupa Prof. Chen

Similar documents
Chapter 9 Practical cycles

ME 200 Final Exam December 12, :00 a.m. to 10:00 a.m.

ME 200 Final Exam December 14, :00 a.m. to 10:00 a.m.

FINAL EXAM. ME 200 Thermodynamics I, Spring 2013 CIRCLE YOUR LECTURE BELOW:

ME 200 Thermodynamics I, Spring 2015, Exam 3, 8 p.m. to 9 p.m. on April 14, 2015

ME 200 Exam 2 October 16, :30 p.m. to 7:30 p.m.

EXAM # 1 CIRCLE YOUR LECTURE BELOW: 8:30 am 11:30 am 2:30 pm Prof. Memon Prof. Naik Prof. Lucht INSTRUCTIONS

EXAM # 1 ME 300 SP2017

ME 200 Exam 2 October 22, :30 p.m. to 7:30 p.m.

Efficiencies. Damian Vogt Course MJ2429. Nomenclature. Symbol Denotation Unit c Flow speed m/s c p. pressure c v. Specific heat at constant J/kgK

Last Name: First Name: Purdue ID: Please write your name in BLOCK letters. Otherwise Gradescope may not recognize your name.

8:30 am 11:30 am 2:30 pm Prof. Memon Prof. Naik Prof. Lucht

(1)5. Which of the following equations is always valid for a fixed mass system undergoing an irreversible or reversible process:

(b) The heat transfer can be determined from an energy balance on the system

ME 354 THERMODYNAMICS 2 MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number: Instructions

Engineering Services Examination - UPSC MECHANICAL ENGINEERING. Topic-wise Conventional Papers I & II (Last 30 Years Questions)

ECE309 THERMODYNAMICS & HEAT TRANSFER MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number:

I affirm that I have never given nor received aid on this examination. I understand that cheating in the exam will result in a grade F for the class.

Course: MECH-341 Thermodynamics II Semester: Fall 2006

Refrigeration. 05/04/2011 T.Al-Shemmeri 1

Unit code: H/ QCF level: 5 Credit value: 15 OUTCOME 1 - THERMODYNAMIC SYSTEMS TUTORIAL 2

SPC 407 Sheet 6 - Solution Compressible Flow Fanno Flow

MAE 320 HW 7B. 1e. For an isolated system, please circle the parameter which will change with time. (a) Total energy;

Session 12 : Monopropellant Thrusters

Name: Discussion Section:

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics

Chemistry 531 Spring 2009 Problem Set 6 Solutions

MAE 320 THERODYNAMICS FINAL EXAM - Practice. Name: You are allowed three sheets of notes.

10 th Jubilee National Congress on Theoretical and Applied Mechanics, Varna September 2005

Improving the performance of geothermal power plant by substituting water steam power plant for the binary power plant

Chapter 20: Exercises: 3, 7, 11, 22, 28, 34 EOC: 40, 43, 46, 58

Name: Discussion Section:

SIMPLE RANKINE CYCLE. 3 expander. boiler. pump. condenser 1 W Q. cycle cycle. net. shaft

δq T = nr ln(v B/V A )

Study of the circulation theory of the cooling system in vertical evaporative cooling generator

Chapter 1 Fundamentals

Roots Blower with Gradually Expanding Outlet Gap: Mathematical Modelling and Performance Simulation Yingjie Cai 1, a, Ligang Yao 2, b

Name: Student Number: PRINT family name first UNIVERSITY OF VICTORIA EXAMINATIONS DECEMBER Chemistry 245 Introductory Physical Chemistry

Calculators are permitted. Computers, PDAs, and other electronic devices with a keyboard are not. Cell phones may not be used as calculators.

Lecture 44: Review Thermodynamics I

Equilibrium point of any reaction is characterized by a single number: K eq is the equilibrium constant for the reaction

Availability and Irreversibility

ME 354 Tutorial, Week#13 Reacting Mixtures

Name: I have observed the honor code and have neither given nor received aid on this exam.

ME 315 Exam 3 8:00-9:00 PM Thursday, April 16, 2009 CIRCLE YOUR DIVISION

The extreme case of the anisothermal calorimeter when there is no heat exchange is the adiabatic calorimeter.

AT 25 C! CH10090 Thermodynamics (part 2) Enthalpy changes during reactions. Let s remember what we did in CH10089

Thermodynamics Qualifying Exam Study Material

UBMCC11 - THERMODYNAMICS. B.E (Marine Engineering) B 16 BASIC CONCEPTS AND FIRST LAW PART- A

I have not proofread these notes; so please watch out for typos, anything misleading or just plain wrong.

ME 200 Thermodynamics 1 Fall 2017 Exam 3

Why do Golf Balls have Dimples on Their Surfaces?

02. Equilibrium Thermodynamics II: Engines

NODIA AND COMPANY. GATE SOLVED PAPER Mechanical Engineering Thermodynamics. Copyright By NODIA & COMPANY

Theory of turbomachinery. Chapter 1

Chapter 2 Solutions. 2.1 (D) Pressure and temperature are dependent during phase change and independent when in a single phase.

Phase transition. Asaf Pe er Background

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES

Name: Discussion Section:

Engineering Mathematics (E35 317) Final Exam December 15, 2006

Internal Energy in terms of Properties

Chapter-6: Entropy. 1 Clausius Inequality. 2 Entropy - A Property

FUGACITY. It is simply a measure of molar Gibbs energy of a real gas.

Physics 2A (Fall 2012) Chapters 11:Using Energy and 12: Thermal Properties of Matter

Chemical Engineering Thermodynamics Spring 2002

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

ECE309 INTRODUCTION TO THERMODYNAMICS & HEAT TRANSFER. 20 June 2005

Introduction To Resonant. Circuits. Resonance in series & parallel RLC circuits

5/6/ :41 PM. Chapter 6. Using Entropy. Dr. Mohammad Abuhaiba, PE

PV/T = k or PV = kt Describe the difference between an ideal gas and a real gas.

Lecture 38: Vapor-compression refrigeration systems

ME Thermodynamics I. Lecture Notes and Example Problems

Chapter 5. Mass and Energy Analysis of Control Volumes. by Asst. Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn

ANALYTICAL MODEL FOR THE BYPASS VALVE IN A LOOP HEAT PIPE

ME 300 Thermodynamics II Spring 2015 Exam 3. Son Jain Lucht 8:30AM 11:30AM 2:30PM

Lecture 37. Heat of Reaction. 1 st Law Analysis of Combustion Systems

MAHALAKSHMI ENGINEERING COLLEGE

first law of ThermodyNamics

Name: Discussion Section:

Number of extra papers used if any

Lecture 35: Vapor power systems, Rankine cycle

ME 200 Thermodynamics 1 Fall 2016 Final Exam

I. (20%) Answer the following True (T) or False (F). If false, explain why for full credit.

Actual exergy intake to perform the same task

Thermodynamics in combustion

Readings for this homework assignment and upcoming lectures

Liquid water static energy page 1/8

300 kpa 77 C. (d) If we neglect kinetic energy in the calculation of energy transport by mass

/ p) TA,. Returning to the

COMBUSTION OF FUEL 12:57:42

a b c d e GOOD LUCK! 3. a b c d e 12. a b c d e 4. a b c d e 13. a b c d e 5. a b c d e 14. a b c d e 6. a b c d e 15. a b c d e

Chapter 7 Energy Principle

Performance Prediction of Solar Thermal Parabolic Trough Concentrator System (STPTCS) by Enhancement of Heat Transfer

( ) Chapter 12. Problem Problem Problem 12.3 G = T = 0 T = K. Mg CO3 = Mg O + CO2. We know that ( ) 10 amt

Ideal Gas Law. September 2, 2014

Find: a) Mass of the air, in kg, b) final temperature of the air, in K, and c) amount of entropy produced, in kj/k.

The Second Law: The Machinery

Basic Thermodynamics Module 1

Transcription:

CIRCLE YOUR LECURE BELOW: Div. 1 10:30 am Div. :30 m Div. 3 4:30 m Prof. Gore Prof. Udua Prof. Chen EXAM # 3 INSRUCIONS 1. his is a closed book examination. All needed roerty tables are rovided.. Do not hesitate to ask the instructor if you do not understand a roblem statement. 3. Start each roblem on the same age as the roblem statement. Write on only one side of the age. Materials on the back side of the age ill not be graded. here are blank ages rovided for your ork. 4. Put only one roblem on a age. A second roblem on the same age ill not be graded. 5. Label your system and list relevant assumtions for roblems and 3. 6. If you give multile solutions, you ill receive only a artial credit although one of the solutions is correct. Delete the solutions you do not ant. 7. For your on benefit, lease rite clearly and legibly. Maximum credit for each roblem is indicated belo. 8. After you have comleted the exam, at your seat, ut your aers in order. his may mean that you have to remove the stale and re-stale. Do not turn in loose ages. 9. Once time is called you ill have three minutes to turn in your exam. Points ill be subtracted for exams turned in after these three minutes. 10. Use calculators authorized by the School of Mechanical Engineering. Problem Possible Score 1 40 30 3 30 otal 100 1

Problem 1. (40 oints) Anser the folloing short-anser questions. You must sho ork and/or rovide an exlanation to receive credit. a) Consider to vaor-comression refrigeration cycles. he refrigerant enters the throttling valve as a saturated liquid at 30 o C in one cycle and as a subcooled liquid at 8 o C in the other. Both cycles oerate ithin the same ressure range. Which cycle ill have a higher COP? Use a -s and/or P-h diagram to exlain. You can assume that liquid enthaly only deends on temerature. 3b 3a 3b 3a 4b 4a 1 4b 4a 1 s h Cycle 1--3b-4b (ith subcooled liquid entering the throttle ill have a higher COP than the cycle 1--3a-4a because for identical amount of ork inut, the former has a higher heat removed from the refrigerated material (hich is at tem. designated by the red dashed line). b) A heat um oerates ith a condenser temerature of 7 o C and delivers heat to a house maintained at 17 o C. he evaorator of this heat um oerates at an average temerature of 3 o C and the environment is at 13 o C. Find the maximum COP and the maximum second la efficiency of the heat um. COPmax-HP = H/(H-L) = (73+7)/(7-3) = 1.5 COPmax-revHP = H-house/(H-house-Lenv) = (73+17)/(17-13) = 7.5 Second La Efficiency = COPmax-HP/COPmax-rev= (1.5/7.5) (100)= 17.4%

c) Considering the definition of molar enthaly of secies k defined in the standard equation o sheet as: h () h (98) h () h (98), state if the folloing statements are k f,k s,k s,k RUE/FALSE? Exlain. N A) he term n k h s,k() h s,k(98) of an exhaust gas mixture leaving a combustor k 1 deends on the number of moles of each secies and the temerature of the mixture. B) he term N k 1 nh (98) of an exhaust gas mixture deends on the on the number k o f,k ofmoles of each secies and the temerature of the mixture. A) RUE because sensible energy does deend on the number of mols and temerature of each secies and the temerature is equal for all secies and is equal to the mixture temerature. B) FALSE because the heat of formation does not deend on the temerature of the mixture but only on the reference temerature. d) What is the difference beteen the Engineering Equations Solver (EES) statement (A) and EES statement (B) belo? (A) hb enthaly( H O, 1 ) (B) hd enthaly(ater, 1, P P1) (A) Gives the enthaly of HO considered as an ideal gas at temerature of 1. (B) Gives the enthaly of liquid ater at a temerature of 1 and a ressure of P1. e) A mixture of O N NOin equilibrium at a certain temerature and ressure is isothermally comressed to tice the ressure. Considering only the single equilibrium reaction, O N NOill the number of moles of each individual secies change if the ressure is increased? Exlain. he number of moles of each individual secies ill not change since the temerature is constant the quantity PNOPNO/POPN = nno nno (N) (N)/nO nn (N) (N) = nno nno / no nn is constant since N the total moles cancel out from the numerator and the denominator. 3

Problem. (30 oints) A Rankine vaor oer cycle oerates ith ater as the orking fluid. Saturated liquid leaves the condenser at 60 o C, and saturated vaor enters the turbine at 00 o C. he turbine oerates in an isentroic manner, hile the um has an isentroic efficiency of 0.8. Assume the corresonding Carnot cycle oerates beteen 60 o C and 00 o C. (Given: the secific enthaly at the turbine exit is 114.3 kj/kg) Find: (1) State your assumtions and dra the cycle on a -s diagram. () Determine the thermal efficiency. (3) Determine the nd la efficiency. (1) Assumtions: Steady-state steady flo No change in kinetic energy and otential energy -s diagram: 1s 1 4 3 s () Using thermodynamic data (Provided on cover hoto) and given definition of states: o 00 C 1 1s 15.54bar, h 793.kJ/kg o 3 4 3 60 C 4 3 0.1994bar, h4 51.13kJ/kg, v 4=0.001017m /kg Pum (4 to 1): 3 3 m 100kJ/m,s v 4(1s 4) 0.001017 (15.54 0.1994)bar 1.56kJ / kg kg 1bar,s 1.56kJ / kg 1.95kJ / kg 0.8 h1 h4 h1 h 4 (1.95 51.13) 53.08kJ / kg 4

Boiler (1 to ): q h h (793. 53.08)kJ / kg 540.1kJ / kg in 1 urbine ( to 3): From given in roblem statement: h3 114.3kJ / kg h h 3 (793. 114.3)kJ/kg=678.88kJ/kg hermal efficiency: (678.88 1.95)kJ/kg th 6.6% q 540.1kJ / kg in (3) Carnot cycle efficiency: L (60 73)K C 1 1 9.6% (00 73)K H nd la efficiency: th 6.6% 89.9% 9.6% C 5

Problem 3. (30 oints) he combustion roducts from burning one mole of entane, ith ure oxygen in a stoichiometric ratio exit at 400 K, 100 kpa. (a) Determine the coefficients a, b and c in the stoichiometric reaction belo Next, consider the dissociation of only. (b) What is the equilibrium constant for the reaction shon belo at 400 K 1 (c) It is observed that 0.4 moles of are resent in the exhaust, of an actual combustor, for every mole of entane that as burnt. Write a balanced equation for the actual reaction. Ho many moles of and are resent in the exhaust? (d) If the exhaust in art (c) continues to react, hich direction is the dissociation of reaction (described in art (b) likely to roceed, forard or backard, to attain equilibrium? Solution: a. 8 5 6 b. Referring to table on cover age, the equilibrium constant is, log 1.679 0.01 c. 8 6 0.4 Balancing C: 5 0.4 4.6 Balancing O: 16 0.4 6 0. herefore, number of moles of CO is 4.6 moles and number of moles of O is 0... d. 0.0357... 0.0179 0.41. / 0.0116 Since this is less than K calculated in art b, the reaction ill move forard to roduce more CO. 6