ENVIRONMENTAL PROTECTION AGENCY. APTI 413: Control of Particulate Matter Emissions. Student Manual: Chapter 1

Size: px
Start display at page:

Download "ENVIRONMENTAL PROTECTION AGENCY. APTI 413: Control of Particulate Matter Emissions. Student Manual: Chapter 1"

Transcription

1 ENVIRONMENTAL PROTECTION AGENCY APTI 41: Control of Particulate Matter Emissions Student Manual: Chater 1

2 A P T I : 4 1 C O N T R O L O F P A R T I C U L A T E M A T T E R E M I S S I O N S, 5 T H E D I T I O N Student Manual C 2 Technoloies, Inc Fountain Way Suite 200 Newort News, VA 2606 Phone Fax The rearation of this manual was overseen by the oranizations of the Environmental Protection Aency (EPA) and the National Association of Clean Air Aencies (NACAA*), and the revision of materials was coordinated and manaed by the Tidewater Oerations Center of C 2 Technoloies, Inc., Newort News, Virinia. Valuable research and feedback was rovided by an advisory rou of subject matter exerts comosed of Dr. Jerry W. Crowder, TX; Dr. Tim Keener, OH; Dr. Doulas P. Harrison, LA., and Mr. Tim Smith, Senior Air Quality Secialist, EPA, Office of Air Quality Plannin and Standards. Acknowledements and thanks are also extended to Ruters University, esecially Francesco Maimone, Co-Director of the Ruters Air Pollution Trainin Proram, which hosted the ilot of the revised materials, and the additional reference sources that can be found throuhout the manuals. *The National Association of Clean Air Aencies (NACAA) reresents air ollution control aencies in 5 states and territories and over 165 major metroolitan areas across the United States. State and local air ollution control officials formed NACAA (formerly STAPPA/ALAPCO) over 0 years ao to imrove their effectiveness as manaers of air quality rorams. The associations serve to encourae the exchane of information amon air ollution control officials, to enhance communication and cooeration amon federal, state, and local reulatory aencies, and to romote ood manaement of our air resources.

3 Table of Contents Basic Concets Gas Temerature... 1 Absolute Temerature... 2 Standard Temerature Gas Pressure... Barometric Pressure... Gaue Pressure... Absolute Pressure Molecular Weiht and the Mole Equation of State... 5 Volume Correction... 6 Molar Volume... 7 Gas Density Viscosity... 8 Liquid Viscosity... 9 Gas Viscosity... 9 Kinematic Viscosity Reynolds Number Calculation of Dew Point Review Questions Review Question Answers Review Problems Review Problem Solutions References... 19

4 Chater 1 This chater will take aroximately 2.5 hours to comlete. O B J E C T I V E S Terminal Learnin Objective At the end of this overview chater, the student will be able to understand basic science concets necessary for the control of articulate matter emissions. Enablin Learnin Objectives 1.1 Distinuish between two tyes of as temerature. 1.2 Distinuish between three tyes of as ressures. 1. Calculate the molecular weiht of as mixtures. 1.4 Identify the five arameters in the Ideal Gas Law. 1.5 Distinuish between the two tyes of viscosity. 1.6 Define two tyes of Reynolds Number. 1.7 Calculate Dew Point Basic Concets This chater distinuishes the basic concet used to reulate articulate matter emissions by examinin various control concets and methods. 1.1 Gas Temerature There are several scales available for measurin temerature. The Fahrenheit scale and the Celsius or Centirade scale, both of which are based on the roerties of water, are the two most commonly used scales for measurin temeratures. As shown below in Fiure 1-1, the Fahrenheit scale searates the freezin and boilin oints into 180-deree units. The Fahrenheit scale sets the freezin temerature of water at 2 F, and the normal boilin temerature of water at 212 F. The Celsius scale searates the freezin and boilin oints into 100-deree units. The Celsius scale sets the freezin temerature of water at 0 C and the normal boilin temerature at 100 C. The followin relationshis convert one scale to another: (1-1) (1-2) F 1.8 C + 2 F 2 C 1.8 Checks on Learnin End of Chater Review Fiure 1.1 In this course, the USEPA standard temerature of 68 F will be used 1

5 Absolute Temerature Fahrenheit and Celsius scales can be used in daily ractices, but both create difficulties when formin temerature ratios or when takin roots and owers of neative temeratures. The best resolve to these situations is an absolute temerature scale, which is a scale with zero set as its lowest value. Exeriments with ideal ases have shown that, under constant ressure, for each chane in Fahrenheit deree below 2 F the volume of as chanes 1/ Similarly, for each Celsius deree below 0 C the volume chanes 1/ Therefore, if this chane in volume er temerature deree is constant, then theoretically the volume of as would become zero at Fahrenheit derees below 2 F, or at F. On the Celsius scale, this condition occurs at Celsius derees below 0 C or at a temerature of C. Absolute temeratures determined by usin Fahrenheit units are exressed as derees Rankine ( R). Absolute temeratures determined by usin Celsius units are exressed as Kelvin (K). As shown below in Fiure 2-2 the followin aroximate relationshis convert one scale to the other: (1- & 1-4) R F K C + 27 Standard Temerature There is not a common temerature that is reconized by all rous. One articular temerature of interest is standard temerature. USEPA has two standard temeratures, one for air monitorin, and one for all other alications. The standard temeratures used by various rous are listed in Table 1-1. Table 1-1 Standard Temeratures Grou Tstd USEPA (General) 68 F (20 C) USEPA (Air monitorin) 77 F (25 C) Industrial hyiene 70 F (21.1 C) Combustion 60 F (15.6 C) Science 2 F (0 C) Examle 1-1 The as temerature in the stack of a wet scrubber system is 10 F. What is the absolute temerature in Rankine and Kelvin? 2

6 Solution Absolute Tem. R 460 R + 10 F 590 R 590 R Absolute Tem. K K 1.2 Gas Pressure A body may be subjected to three kinds of stress: shear, comression, and tension. Fluids are unable to withstand tension stress; therefore, they are subject only to shear and comression stress. Unit comressive stress in a fluid is termed ressure and is exressed as force er unit area (e.., lb f /in 2 and Newtons/m 2 ). Pressure is equal in all directions at a oint within a volume for fluid and acts erendicular to a surface. Barometric Pressure Barometric ressure and atmosheric ressure are synonymous. These ressures are measured with a barometer and are usually exressed as inches or millimeters of mercury (H). Standard barometric ressure is internationally reconized and is the averae atmosheric ressure at sea level, 45 N latitude and at 5 F. Standard barometric ressure is equivalent to a ressure of ounds force er square inch exerted at the base of a column of mercury inches hih. Other equivalents to standard ressure are listed in Table 1-2. Weather and altitude are resonsible for barometric ressure variations. Table 1-2. Standard Pressure Units Value Atmoshere (atm) 1 Pounds force er square inch (si) Inches of mercury (in H) Millimeters of mercury (mm H) 760 Feet of water column (ft WC).92 Inches of water column (in WC) 407 Kiloascals (kpa) 101. Millibars (mb) 101 Gaue Pressure The ressure inside an air ollution control system is termed the aue or static ressure and is measured relative to the revailin atmosheric ressure, as shown in Fiure 1-2. If the system ressure is reater than the atmosheric ressure, then the aue ressure is exressed as a ositive value. If the system ressure is smaller, then the aue ressure is exressed as a neative value. The term vacuum desinates a neative aue ressure. Gaue or static ressures in air ollution systems are usually exressed in inches of water column (in WC).

7 Fiure 1-2. Definition of ositive and neative aue ressures. Absolute ressure the alebraic sum of the atmosheric ressure and the aue ressure. Absolute Pressure The aue ressures commonly used in reference to air ollution control systems share an attribute that causes difficulties in the use of normal temerature scales they can have neative values. As a result, calculations involvin ressure ratios and roots and owers of ressure must use absolute ressure. Absolute ressure is the alebraic sum of the atmosheric ressure and the aue ressure: (1-5) P P b + P Where P absolute ressure P b barometric or atmosheric ressure P aue ressure An air ollution control device has an inlet static ressure of -25 in Examle 1-2 WC. What is the absolute static ressure at the inlet of the air ollution control device if the barometric ressure at the time is in H? Solution Convert the barometric ressure units to in WC : 407 in WC Pb in H 406 in WC in H Add the barometric and aue (static) ressures : P 406 in WC + (-25 in WC) 81in WC 1. Molecular Weiht and the Mole The molecular weiht of a comound is the sum of the atomic weihts of all the atoms in the molecule. The atomic weiht of an atom is based on an arbitrary scale of the relative masses of the elements, usually based on a carbon value of 12. The chemical identity of an atom is determined by the number of rotons in its nucleus and is called the atomic number. Values of atomic number and atomic weiht can be found in a Periodic Table of Elements. 4

8 Mixtures of molecules do not have a true molecular weiht; however, they do have an aarent molecular weiht that can be calculated from the comosition of the mixture: Periodic Table htt://education.jlab.or /beamsactivity/6thra de/tableofelements/stu 01.l.html Moles can be exressed in terms of any mass unit: ram-moles, kiloram-moles, ouncemoles, ound-moles and ton-moles (1-6) MW mixture n i 1 χ i MW where χ i is the mole fraction of comonent i and MW i is its molecular weiht. Proerties of a contaminated as can be aroximated by the roerties of air, which is itself a mixture of molecules. The aarent molecular weiht of air is 28.95, or aroximately 29. A mole is a mass of material that contains a certain number of molecules. Moles can be exressed in terms of any mass unit; thus, e.., there are ram-moles, kiloram-moles, ounce-moles, ound-moles and ton-moles. The relationshi between the different tyes of moles is the same as the relationshi between the corresondin mass units. Thus, there are 1,000 ram-moles in a kiloram-mole, 45.6-ram-moles in a oundmole, 16 ounce-moles in a ound-mole and 2,000 ound-moles in a ton-mole. The ram-mole is the mass of material that contains Avoadro's number of molecules, aroximately 6.02 x The mass of a mole is numerically equal to the molecular weiht. For oxyen, which has a molecular weiht of 2, there are 2 rams er rammole, 2 kilorams er kiloram-mole, and 2 ounds er-ound mole. However, only the ram-mole contains Avoadro's number of molecules. The kiloram-mole contains 1,000 times Avoadro's number of molecules; the ound-mole contains 45.6 times. i 1.4 Equation of State Equations of state relate the ressure, volume, and temerature roerties of a ure substance or mixture by semi-theoretical or emirical relationshis. Over the rane of temerature and ressure usually encountered in air ollution control systems, these values may be related by the ideal or erfect as law: (1-7) Where P absolute ressure V as volume n number of moles R as constant T absolute temerature PV nrt Here, R is referred to as the universal as constant, and its value deends on the units 5

9 of the other terms in the equation. Values of R include: 10.7sia ft /lb mole R 0.7atm ft /lb mole R atm cm / mole K 8.1x 10 kpa m /k mole K Volume Correction A useful relationshi can be develoed from the ideal as law by notin that PV/T nr, and that, for a iven number of moles of a as, nr is a constant. Thus, at two different conditions for the same as, we may write equation 1-8. Equation 1-9 allows volumes (or volumetric rates) to be corrected from one set of temerature and ressure conditions to another. One common calculation (1-10) is to convert volumetric flow rate from actual conditions to standard conditions, or vice versa (1-11). SCFM standard cubic feet er minute ACFM actual cubic feet er minute (1-8) (1-9) (1-10) (1-11) 1 P1 V1 T 1 V V 2 P2V T P SCFM ACFM P P ACFM SCFM P 2 2 P 2 T1 P1 T2 actual std std actual T T std actual T T actual std Examle 1- A articulate control system consists of a hood, ductwork, fabric filter, fan, and stack. The total as flow enterin the fabric filter is 8,640 scfm. The as temerature in the inlet duct is 20 F and the static ressure is -10 in WC. The barometric ressure is 28.0 in H. If the inlet duct has inside dimensions of feet by 4 feet, what is the velocity into the fabric filter? 6

10 Solution Convert the static ressure to absolute ressure : 407 in WC P 28.0in H ( 10 in WC) 75 in in H + WC Convert the as temerature to T actual 20 F R absolute temerature : Convert the inlet flow rate to actual conditions : Q actual 780 R 407in WC 8,640scfm 1,85acfm 528 R 75in WC Calculate the velocity: 1,85 ft V min 1,154 ft ft 4ft min Molar Volume The ideal as law can also be rearraned to calculate the volume occuied by a mole of as, called the molar volume: (1-12) Examle 1-4 V RT n P What is the molar volume of an ideal as at 68 F and 1 atm? At 200 F and 1 atm? Solution At68 Fand1atm : V n RT P atm ft 0.7 lb mole R 1atm ( 528 R) 85.4 ft lb mole At 200 F and 1 atm : V n or RT P atm ft 0.7 lb mole R 1atm ( 660 R) ft lb mole Gas Density V 660 R ft n 528 R lb mole 7

11 D E S I G N C U S T O M I Z A T I O N Finally, we can use the ideal as law to estimate as density. Density is the ratio of the mass of a material to the volume that material occuies. For accurate values, as densities should be determined from reference texts. However, an estimate of the as density can be determined from the ideal as law. Reconizin that the number of moles is iven by mass (m) divided by molecular weiht (MW), the ideal as law may be written: Gas Viscosity increases with an increase in temerature. (1-1) PV m MW The as density (ρ) can then be estimated from: RT (1-14) ρ m v P MW RT (1-15) Density can also be estimated from the molecular weiht and molar volume: MW 85.4 ρ Where Ρ absolute ressure (in H) Τ absolute temerature ( R) 1.5 Viscosity 528 T P Viscosity is the roerty associated with a fluid resistance to flow. Viscosity is the result of two henomena: (1) intermolecular cohesive forces and (2) momentum transfer between flowin strata caused by molecular aitation erendicular to the direction of motion. Between adjacent strata of a movin Newtonian fluid, a shearin stress, σ, occurs that is directly roortional to the velocity radient or shear rate, Γ (see Fiure 1-). This is exressed in the equation: (1-16) σ Γ dv dy Where σ shear stress roortionality constant Γ shear rate or velocity radient (dv/dy)

12 The roortionality constant,, is called the coefficient of viscosity, the absolute viscosity or merely viscosity. It should be noted that the ressure does not aear in Equation 1-16, indicatin that the shear stress and viscosity are indeendent of ressure. Actually, viscosity increases very slihtly with ressure, but this variation is neliible in most enineerin calculations. Fiure 1-. Shearin stress in a movin fluid Liquid Viscosity decreases with an increase in temerature. Liquid Viscosity In a liquid, transfer of momentum between strata flowin at slihtly different velocities is small comared to the cohesive forces between molecules. Hence, viscosity in liquids is redominantly the result of intermolecular cohesion. Because forces of cohesion decrease raidly with an increase in temerature, liquid viscosity decreases with an increase in temerature. Gas Viscosity In a as, the molecules are too far aart for intermolecular cohesion to be effective. Thus, the viscosity in ases is redominantly the result of an exchane of momentum between flowin strata caused by molecular transfer. Since molecular motion increases as temerature increases, as viscosity increases with an increase in temerature. The viscosity of air at any temerature may be estimated from: (1-17) Where absolute viscosity T ref T ref ref absolute viscosity at reference temerature Τ absolute temerature reference absolute temerature Τ ref 9

13 The viscosity of air containin other ases imortant in air ollution control alications can also be estimated from: (1-18) Τ +.24 x 10-5 Τ x y Where absolute viscosity (microoise) Τ absolute temerature x water vaor content (fraction) y oxyen content (fraction) The viscosity of air at 68 F is 1.21 x 10-5 lb m /ft. sec or 1.8 x 10-4 /cm sec Kinematic Viscosity The ratio of the absolute viscosity to the density of a fluid, known as kinematic viscosity, often aears in dimensionless numbers, such as the Reynolds Number. Kinematic viscosity is defined accordin to the followin relationshi and is used to simlify calculations: Dimensionless numbers htt:// extract8.htmltemerature. htt://en.wikiedia.or/wiki/ Dimensionless_numbers (1-19) Where υ kinematic viscosity absolute viscosity ρ density viscosity v ρ Reynolds Number Is the ratio of inertial forces to viscous forces in a flowin fluid. Reynolds Number Reynolds Number is the ratio of inertial forces to viscous forces in a flowin fluid. A tyical inertial force er unit volume of fluid is ρν 2 /L. A tyical viscous force er unit volume of fluid is ν/l 2. The first exression divided by the second rovides the dimensionless ratio known as the Reynolds Number: (1-20) Re Lvρ Where Re Reynolds Number L characteristics system dimension ν fluid velocity ρ fluid density fluid viscosity 10

14 The linear dimension, L, is a lenth characteristic of the flow system. It is equal to four times the mean hydraulic radius, which is the cross-sectional area divided by the wetted erimeter. Thus, for a circular ie, L is the ie diameter, D, and the Reynolds Number (sometimes termed the Flow Reynolds Number) takes the form: (1-21) Re Dvρ Particle Motion Most article motion in air ollution control devices occurs in the Stokes and Transitional Reions. Reynolds Number in this form is used to distinuish between laminar and turbulent flow. In laminar flow, the fluid is constrained to motion in layers, or laminae, by the action of viscosity. These layers of fluid move in arallel aths that remain distinct from one another. Laminar flow occurs when the Reynolds Number is less than about 2,000. In turbulent flow, the fluid is not restricted to arallel aths but moves forward in a random, chaotic manner. Fully turbulent flow occurs when the Reynolds Number is reater than about,000. Between Reynolds Numbers of 2,000 and,000, the flow may be laminar or turbulent, deendin on the flow system conditions. Pie or duct vibration, for examle, can cause turbulent conditions to exist at Reynolds Numbers sinificantly below,000. It is worth notin that, rimarily because of the size, flow in air ollution control equiment is always turbulent. Laminar conditions are resent only in the very thin boundary layers that form near surfaces. A form of Reynolds Number that is of reater interest in this course is the Particle Reynolds Number. Here, the characteristic system dimension is the article diameter, d, and the velocity, v, is the article velocity relative to the as stream: (1-22) Re Particle Reynolds Number is used to characterize flow conditions when articles move throuh or with a flowin fluid. Particle Reynolds Numbers less than about one indicate laminar conditions and define what is commonly termed the Stokes Reion. Values over about 1,000 indicate turbulent conditions and define what is commonly termed the Newton Reion. Particle Reynolds Numbers between 1 and 1,000 indicate transitional conditions. Most article motion in air ollution control devices occurs in the Stokes and Transitional Reions. Examle 1-5 Calculate the Particle Reynolds Number for a 2m diameter article movin throuh 10 C still air at a velocity of 6 m/sec. Solution From Aendix B, the density of air at 20 C is 1.20 x 10 - /cm and the viscosity is 1.80 x 10-4 /cm(sec) D v ρ 11

15 Estimate the as density at10 C. 29K ρ 1.20x x10 28K Estimate the as vicosity at10 C. 4 29K 1.80x x10 28K CalculateParticle Reynolds Number : Re d v ρ (2x cm) 2 ( 6x10 cm ) 1.75x10 cm 4 4 cm sec 1.24x10 sec cm sec cm Examle 1-6 Calculate the Particle Reynolds Number for a as stream movin throuh a 200 cm diameter duct at a velocity of 1,500 cm/sec. Assume that the articles are movin at the same velocity as the as stream and are not settlin due to ravity. Assume a as temerature of 20 C and standard ressure. Solution Since there is no difference in velocity between the as stream and the article, the Particle Reynolds Number is zero. The Flow Reynolds Number is: 1.20x10 sec Dvρ cm Re 2.00x x10 cm sec ( 200cm)( 1,500 cm ) 6 Why is Dew Point imortant? This condensate can form aste on fabric filters makin them unusable 1.7 Calculation of Dew Point Many as streams that must be treated for articulate emissions may also contain sinificant amounts of water vaor or another condensable comonent. In most cases, for examle, if articulate control is to be accomlished usin fabric filters, it is necessary that the as stream be maintained at a temerature sufficient to revent the water or other comonent from condensin as condensation will cause the articulate matter to collect on the filters as a aste that cannot be easily cleaned. The temerature at which condensation occurs is also known as the dew oint temerature. At the dew oint temerature the artial ressure of the condensable comonent is equal to its vaor ressure 12

16 Where Ρ i P * yρ P i artial ressure of the condensable comonent P* vaor ressure of the condensable comonent y i mole fraction of the condensable comonent in the as P total ressure Vaor ressure as a function of temerature can be obtained from the Antoine equation. Where B lo 10 P* A T + C P* vaor ressure, m H T Temerature, C A, B, and C are unique constants for each comonent Tables of Antoine constants may be found in numerous standard references and is offered in Aendix C. i For water, values of the vaor ressure as a function of temerature may be obtained directly from Vaor Pressure Tables (available widely on the internet. Examle 1-7 The mol fraction of water in the stack as from a combustion rocess contains 14 mol% water vaor. What is the dew oint temerature if the total ressure is 1 atm? The Antoine constants for water are: Where to see Steam Tables htt://ye.dyndns.or/fre esteam/ Solution A B C At the dew oint temerature: P* P i y i P 0.14 (1) 0.14 atm or mmh From the Antoine equation: lo 10 P* T Solve for T to obtain: T 5 C 1

17 Review Questions 1. How does the article Reynolds number chane when the as temerature is increased? a. Increases b. Decreases c. Remains unchaned 2. How does the as viscosity chane as the temerature is increased? a. Increases b. Decreases c. Remains unchaned. Flow in air ollution control equiment is always turbulent, and Laminar conditions are only resent in the very thin boundary layers that form near surfaces. a. True b. False 4. When Particle Reynolds Numbers indicate laminar conditions that exist within the a. Flow Reynolds Reion b. Newton Reion c. Stokes Reion d. Viscous Reion 14

18 Review Question Answers 1. How does the article Reynolds number chane when the as temerature is increased? (see ae 10) b. Decreases 2. How does the as viscosity chane as the temerature is increased? (see ae 9) a. Increases. Flow in air ollution control equiment is always turbulent, and Laminar conditions are only resent in the very thin boundary layers that form near surfaces. (ae 10) a. True 4. When Particle Reynolds Numbers indicate laminar conditions that exist within the c. Stokes Reion 15

19 Review Problems 1. The flows from Ducts A and B are combined into a sinle Duct C. The flow rate in Duct A is 5,000 scfm, the as stream temerature is 50 F and the static ressure is -2 in WC. The flow rate in Duct B is 4,000 acfm, the as stream temerature is 400 F and the static ressure is -5 in WC. What is the flow rate in Duct C? Assume a barometric ressure of in H. (see ae 6) 2. Calculate the Particle Reynolds Numbers for the followin articles. Assume a as temerature of 20 C and a ressure of 1 atm. (see ae 10) a. 10 m article movin at 1 ft/sec relative to the as stream b. 10 m article movin at 10 ft/sec relative to the as stream c. 100 m article movin at 1 ft/sec relative to the as stream d. 100 m article movin at 10 ft/sec relative to the as stream 16

20 Review Problem Solutions 1. The flows from Ducts A and B are combined into a sinle Duct C. The flow rate in Duct A is 5,000 scfm, the as stream temerature is 50 F and the static ressure is -2 in WC. The flow rate in Duct B is 4,000 acfm, the as stream temerature is 400 F and the static ressure is -5 in WC. What is the flow rate in Duct C? Assume a barometric ressure of in H. (see ae 6) Solution Calculate the absolute ressure in Duct B : 407 in WC Ρ 29.15in H + ( 5in WC) 61.5in WC 29.92in H Convert the flow in Duct B to standard conditions : 528 R 61.5in WC QB 4,000acfm 2,181scfm 860 R 407 in WC Combine flows : Q c 5,000 scfm + 2,181scfm 7,181scfm 2. Calculate the Particle Reynolds Numbers for the followin articles. Assume a as temerature of 20 C and a ressure of 1 atm. (see ae 10) a. 10 m article movin at 1 ft/sec relative to the as stream b. 10 m article movin at 10 ft/sec relative to the as stream Solution a & b Re d vρ 4 ( 10x10 cm)( [ 1.0 ft )( 0.48 cm )] sec 1.80x x10 ft cm sec cm 0.20 Re d v ρ 4 ( 10x10 cm)( [ 10.0 ft )( 0.48 cm )] sec 1.80x10 4 cm sec 1.20x10 ft cm 2.02 c. 100 m article movin at 1 ft/sec relative to the as stream d. 100 m article movin at 10 ft/sec relative to the as stream 17

21 Solution c & d Re d v ρ 4 ( 100x10 cm)( [ 1.0 ft )( 0.48 cm )] sec 1.80x10 4 cm sec 1.20x10 ft cm 2.0 Re d v ρ 4 ( 100x10 cm)( [ 10.0 ft )( 0.48 cm )] sec 1.80x10 4 cm sec 1.20x10 ft cm

22 References Cenel, Y.A., and M.A. Boles, Thermodynamics: An Enineerin Aroach, McGraw- Hill, New York, Himmelblau, D.M., Basic Princiles and Calculations in Chemical Enineerin, Prentice-Hall, Enlewood Cliffs,

C H A P T E R 5 ENVIRONMENTAL PROTECTION AGENCY. APTI 413: Control of Particulate Matter Emissions. Student Manual Chapter 5.

C H A P T E R 5 ENVIRONMENTAL PROTECTION AGENCY. APTI 413: Control of Particulate Matter Emissions. Student Manual Chapter 5. Chapter 5 C H A P T E R 5 ENVIRONMENTAL PROTECTION AGENCY APTI 413: Control of Particulate Matter Emissions Student Manual Chapter 5 C H A P T E R 5 A P T I : 4 1 3 C O N T R O L O F P A R T I C U L A

More information

df da df = force on one side of da due to pressure

df da df = force on one side of da due to pressure I. Review of Fundamental Fluid Mechanics and Thermodynamics 1. 1 Some fundamental aerodynamic variables htt://en.wikiedia.org/wiki/hurricane_ivan_(2004) 1) Pressure: the normal force er unit area exerted

More information

Chapter 10: Flow Flow in in Conduits Conduits Dr Ali Jawarneh

Chapter 10: Flow Flow in in Conduits Conduits Dr Ali Jawarneh Chater 10: Flow in Conduits By Dr Ali Jawarneh Hashemite University 1 Outline In this chater we will: Analyse the shear stress distribution across a ie section. Discuss and analyse the case of laminar

More information

Chapter 1 Fundamentals

Chapter 1 Fundamentals Chater Fundamentals. Overview of Thermodynamics Industrial Revolution brought in large scale automation of many tedious tasks which were earlier being erformed through manual or animal labour. Inventors

More information

ONE. The Earth-atmosphere system CHAPTER

ONE. The Earth-atmosphere system CHAPTER CHAPTER ONE The Earth-atmoshere system 1.1 INTRODUCTION The Earth s atmoshere is the gaseous enveloe surrounding the lanet. Like other lanetary atmosheres, it figures centrally in transfers of energy between

More information

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

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential Chem 467 Sulement to Lectures 33 Phase Equilibrium Chemical Potential Revisited We introduced the chemical otential as the conjugate variable to amount. Briefly reviewing, the total Gibbs energy of a system

More information

Ideal Gas Law. September 2, 2014

Ideal Gas Law. September 2, 2014 Ideal Gas Law Setember 2, 2014 Thermodynamics deals with internal transformations of the energy of a system and exchanges of energy between that system and its environment. A thermodynamic system refers

More information

AE301 Aerodynamics I UNIT A: Fundamental Concepts

AE301 Aerodynamics I UNIT A: Fundamental Concepts AE301 Aerodynamics I UNIT A: Fundamental Concets ROAD MAP... A-1: Engineering Fundamentals Reiew A-: Standard Atmoshere A-3: Goerning Equations of Aerodynamics A-4: Airseed Measurements A-5: Aerodynamic

More information

The Second Law: The Machinery

The Second Law: The Machinery The Second Law: The Machinery Chater 5 of Atkins: The Second Law: The Concets Sections 3.7-3.9 8th Ed, 3.3 9th Ed; 3.4 10 Ed.; 3E 11th Ed. Combining First and Second Laws Proerties of the Internal Energy

More information

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

FUGACITY. It is simply a measure of molar Gibbs energy of a real gas. FUGACITY It is simly a measure of molar Gibbs energy of a real gas. Modifying the simle equation for the chemical otential of an ideal gas by introducing the concet of a fugacity (f). The fugacity is an

More information

Compressible Flow Introduction. Afshin J. Ghajar

Compressible Flow Introduction. Afshin J. Ghajar 36 Comressible Flow Afshin J. Ghajar Oklahoma State University 36. Introduction...36-36. he Mach Number and Flow Regimes...36-36.3 Ideal Gas Relations...36-36.4 Isentroic Flow Relations...36-4 36.5 Stagnation

More information

Test Review # 7. Combined Gas Law PV T PV T. Ideal Gas Law PV = nrt. Chemistry H-3: Form TR7.6A

Test Review # 7. Combined Gas Law PV T PV T. Ideal Gas Law PV = nrt. Chemistry H-3: Form TR7.6A Chemistry H-3: Form TR7.6A TEST 9 REVIEW Name Date Period Test Review # 7 ENERGY Calculatin Joules. When you heat a solid, it s temperature enerally oes up. There is a relationship between heat and temperature,

More information

Phase transition. Asaf Pe er Background

Phase transition. Asaf Pe er Background Phase transition Asaf Pe er 1 November 18, 2013 1. Background A hase is a region of sace, throughout which all hysical roerties (density, magnetization, etc.) of a material (or thermodynamic system) are

More information

STATES OF MATTER UNIT 5

STATES OF MATTER UNIT 5 32 32 CHEMISTRY UNIT 5 After studying this unit you will be able to exlain the existence of different states of matter in terms of balance between intermolecular forces and thermal energy of articles;

More information

MODULE 2: DIFFUSION LECTURE NO. 2

MODULE 2: DIFFUSION LECTURE NO. 2 PTEL Chemical Mass Transfer Oeration MODULE : DIFFUSIO LECTURE O.. STEDY STTE MOLECULR DIFFUSIO I FLUIDS UDER STGT D LMIR FLOW CODITIOS.. Steady state diffusion through a constant area Steady state diffusion

More information

Chapter 6. Thermodynamics and the Equations of Motion

Chapter 6. Thermodynamics and the Equations of Motion Chater 6 hermodynamics and the Equations of Motion 6.1 he first law of thermodynamics for a fluid and the equation of state. We noted in chater 4 that the full formulation of the equations of motion required

More information

Chapter 7 Energy Principle

Chapter 7 Energy Principle Chater 7: Energy Princile By Dr Ali Jawarneh Hashemite University Outline In this chater we will: Derive and analyse the Energy equation. Analyse the flow and shaft work. Derive the equation for steady

More information

Thermodynamics in combustion

Thermodynamics in combustion Thermodynamics in combustion 2nd ste in toolbox Thermodynamics deals with a equilibrium state and how chemical comosition can be calculated for a system with known atomic or molecular comosition if 2 indeendent

More information

Where: Where: f Wave s frequency (Hz) c Speed of light ( ms -1 ) Wavelength (m)

Where: Where: f Wave s frequency (Hz) c Speed of light ( ms -1 ) Wavelength (m) in a direction to both of the fields as shown in Figure 1. In wave model, the electromagnetic radiation is commonly associated with wavelength and frequency, exressed mathematically as: c f...(1) f Wave

More information

not to be republished NCERT STATES OF MATTER UNIT 5 INTRODUCTION

not to be republished NCERT STATES OF MATTER UNIT 5 INTRODUCTION 32 CHEMISRY UNI 5 SAES OF MAER After studying this unit you will be able to exlain the existence of different states of matter in terms of balance between intermolecular forces and thermal energy of articles;

More information

An-Najah National University Civil Engineering Departemnt. Fluid Mechanics. Chapter [2] Fluid Statics

An-Najah National University Civil Engineering Departemnt. Fluid Mechanics. Chapter [2] Fluid Statics An-Najah National University Civil Engineering Deartemnt Fluid Mechanics Chater [2] Fluid Statics 1 Fluid Statics Problems Fluid statics refers to the study of fluids at rest or moving in such a manner

More information

(British) (SI) British Metric L T [V] = L T. [a] = 2 [F] = F = 2 T

(British) (SI) British Metric L T [V] = L T. [a] = 2 [F] = F = 2 T Hydraulics ecture # CWR 40 age () ecture # Outline: Review of terminology in fluid mechanics: Energy or work Hydraulic head Bernoulli s aw, Conductivity (examle) ransient & turbulent Friction head loss

More information

ANALYTICAL MODEL FOR THE BYPASS VALVE IN A LOOP HEAT PIPE

ANALYTICAL MODEL FOR THE BYPASS VALVE IN A LOOP HEAT PIPE ANALYTICAL MODEL FOR THE BYPASS ALE IN A LOOP HEAT PIPE Michel Seetjens & Camilo Rindt Laboratory for Energy Technology Mechanical Engineering Deartment Eindhoven University of Technology The Netherlands

More information

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS HET, ORK, ND THE FIRST L OF THERMODYNMIS 8 EXERISES Section 8. The First Law of Thermodynamics 5. INTERPRET e identify the system as the water in the insulated container. The roblem involves calculating

More information

FLOW MEASUREMENT IN CLOSED CONDUIT

FLOW MEASUREMENT IN CLOSED CONDUIT FLOW MEASUREMENT IN CLOSED CONDUIT Closed conduit flow: It is a flow with boundaries and runs full. As in the case of oen channel flow, the surface is not exosed to atmoshere. Since it runs full it is

More information

FE Fluids Review March 23, 2012 Steve Burian (Civil & Environmental Engineering)

FE Fluids Review March 23, 2012 Steve Burian (Civil & Environmental Engineering) Topic: Fluid Properties 1. If 6 m 3 of oil weighs 47 kn, calculate its specific weight, density, and specific gravity. 2. 10.0 L of an incompressible liquid exert a force of 20 N at the earth s surface.

More information

Pressure variation with direction. Pressure variation with location How can we calculate the total force on a submerged surface?

Pressure variation with direction. Pressure variation with location How can we calculate the total force on a submerged surface? Definitions and Alications CVEN Statics: no relative motion between adjacent fluid layers. Shear stress is ero Only ressure can be acting Gravity force acts on the fluid ( body force) Alications: Pressure

More information

MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI

MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI 6113 DEPARTMENT: CIVIL SUB.CODE/ NAME: CE6303/ MECHANICS OF FLUIDS SEMESTER: III UNIT-1 FLUID PROPERTIES TWO MARK QUESTIONS AND ANSWERS 1. Define fluid mechanics.(auc

More information

Chapter 9 Practical cycles

Chapter 9 Practical cycles Prof.. undararajan Chater 9 Practical cycles 9. Introduction In Chaters 7 and 8, it was shown that a reversible engine based on the Carnot cycle (two reversible isothermal heat transfers and two reversible

More information

High speed wind tunnels 2.0 Definition of high speed. 2.1 Types of high speed wind tunnels

High speed wind tunnels 2.0 Definition of high speed. 2.1 Types of high speed wind tunnels Module Lectures 6 to 1 High Seed Wind Tunnels Keywords: Blow down wind tunnels, Indraft wind tunnels, suersonic wind tunnels, c-d nozzles, second throat diffuser, shocks, condensation in wind tunnels,

More information

Determination of Pressure Losses in Hydraulic Pipeline Systems by Considering Temperature and Pressure

Determination of Pressure Losses in Hydraulic Pipeline Systems by Considering Temperature and Pressure Paer received: 7.10.008 UDC 61.64 Paer acceted: 0.04.009 Determination of Pressure Losses in Hydraulic Pieline Systems by Considering Temerature and Pressure Vladimir Savi 1,* - Darko Kneževi - Darko Lovrec

More information

Unit 1: Science Skills, Measurement, and Conversions

Unit 1: Science Skills, Measurement, and Conversions Chemistry Practice test Period: Name: Skare Fall 206 Date: pae of 5 Unit : Science Skills, Measurement, and Conversions Learnin Tarets & Sample Questions Most of what we ve done is in Ch. 3 of your book.

More information

GEF2200 vår 2017 Løsningsforslag sett 1

GEF2200 vår 2017 Løsningsforslag sett 1 GEF2200 vår 2017 Løsningsforslag sett 1 A.1.T R is the universal gas constant, with value 8.3143JK 1 mol 1. R is the gas constant for a secic gas, given by R R M (1) where M is the molecular weight of

More information

Liquid water static energy page 1/8

Liquid water static energy page 1/8 Liquid water static energy age 1/8 1) Thermodynamics It s a good idea to work with thermodynamic variables that are conserved under a known set of conditions, since they can act as assive tracers and rovide

More information

The International Association for the Properties of Water and Steam

The International Association for the Properties of Water and Steam IAP AN5-13(2016) he International Association for the Proerties of ater and team London, United Kindom etember 2013 Advisory Note No. 5: Industrial Calculation of the hermodynamic Proerties of eawater

More information

a) Derive general expressions for the stream function Ψ and the velocity potential function φ for the combined flow. [12 Marks]

a) Derive general expressions for the stream function Ψ and the velocity potential function φ for the combined flow. [12 Marks] Question 1 A horizontal irrotational flow system results from the combination of a free vortex, rotating anticlockwise, of strength K=πv θ r, located with its centre at the origin, with a uniform flow

More information

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

The extreme case of the anisothermal calorimeter when there is no heat exchange is the adiabatic calorimeter. .4. Determination of the enthaly of solution of anhydrous and hydrous sodium acetate by anisothermal calorimeter, and the enthaly of melting of ice by isothermal heat flow calorimeter Theoretical background

More information

Mixture Homogeneous Mixtures (air, sea water ) same composition, no chemical bond components are NOT distinguishable

Mixture Homogeneous Mixtures (air, sea water ) same composition, no chemical bond components are NOT distinguishable BASIC CONCEPTAND DEFINITIONS1 2 THERMODYNAMICS CHAPTER 2 Thermodynamic Concets Lecturer Axel GRONIEWSKY, PhD 11 th of February2019 Thermodynamics study of energy and its transformation describes macroscoic

More information

Theory of turbomachinery. Chapter 1

Theory of turbomachinery. Chapter 1 Theory of turbomachinery Chater Introduction: Basic Princiles Take your choice of those that can best aid your action. (Shakeseare, Coriolanus) Introduction Definition Turbomachinery describes machines

More information

Day 3. Fluid Statics. - pressure - forces

Day 3. Fluid Statics. - pressure - forces Day 3 Fluid Statics - ressure - forces we define fluid article: small body of fluid with finite mass but negligible dimension (note: continuum mechanics must aly, so not too small) we consider a fluid

More information

The thermal wind 1. v g

The thermal wind 1. v g The thermal win The thermal win Introuction The geostrohic win is etermine by the graient of the isobars (on a horizontal surface) or isohyses (on a ressure surface). On a ressure surface the graient of

More information

Modelling heat transfer and fluid flow inside a pressure cooker

Modelling heat transfer and fluid flow inside a pressure cooker 17 th Euroean Symosium on Comuter Aided Process Engineering ESCAPE17 V. Plesu and P.S. Agachi (Editors) 2007 Elsevier B.V. All rights reserved. 1 Modelling heat transfer and fluid flow inside a ressure

More information

Setting up the Mathematical Model Review of Heat & Material Balances

Setting up the Mathematical Model Review of Heat & Material Balances Setting u the Mathematical Model Review of Heat & Material Balances Toic Summary... Introduction... Conservation Equations... 3 Use of Intrinsic Variables... 4 Well-Mixed Systems... 4 Conservation of Total

More information

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

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics PHYS1001 PHYSICS 1 REGULAR Module Thermal Physics Chater 17 First Law of Thermodynamics References: 17.1 to 17.9 Examles: 17.1 to 17.7 Checklist Thermodynamic system collection of objects and fields. If

More information

Homogeneous and Inhomogeneous Model for Flow and Heat Transfer in Porous Materials as High Temperature Solar Air Receivers

Homogeneous and Inhomogeneous Model for Flow and Heat Transfer in Porous Materials as High Temperature Solar Air Receivers Excert from the roceedings of the COMSOL Conference 1 aris Homogeneous and Inhomogeneous Model for Flow and Heat ransfer in orous Materials as High emerature Solar Air Receivers Olena Smirnova 1 *, homas

More information

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

Physics 2A (Fall 2012) Chapters 11:Using Energy and 12: Thermal Properties of Matter Physics 2A (Fall 2012) Chaters 11:Using Energy and 12: Thermal Proerties of Matter "Kee in mind that neither success nor failure is ever final." Roger Ward Babson Our greatest glory is not in never failing,

More information

4. A Brief Review of Thermodynamics, Part 2

4. A Brief Review of Thermodynamics, Part 2 ATMOSPHERE OCEAN INTERACTIONS :: LECTURE NOTES 4. A Brief Review of Thermodynamics, Part 2 J. S. Wright jswright@tsinghua.edu.cn 4.1 OVERVIEW This chater continues our review of the key thermodynamics

More information

Session 12 : Monopropellant Thrusters

Session 12 : Monopropellant Thrusters Session 12 : Monoroellant Thrusters Electrothermal augmentation of chemical rockets was the first form of electric roulsion alied in sace vehicles. In its original imlementation, resistojets were used

More information

Analysis of Pressure Transient Response for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia

Analysis of Pressure Transient Response for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia roceedings World Geothermal Congress 00 Bali, Indonesia, 5-9 Aril 00 Analysis of ressure Transient Resonse for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia Jorge A.

More information

ESCI 342 Atmospheric Dynamics I Lesson 10 Vertical Motion, Pressure Coordinates

ESCI 342 Atmospheric Dynamics I Lesson 10 Vertical Motion, Pressure Coordinates Reading: Martin, Section 4.1 PRESSURE COORDINATES ESCI 342 Atmosheric Dynamics I Lesson 10 Vertical Motion, Pressure Coordinates Pressure is often a convenient vertical coordinate to use in lace of altitude.

More information

16. CHARACTERISTICS OF SHOCK-WAVE UNDER LORENTZ FORCE AND ENERGY EXCHANGE

16. CHARACTERISTICS OF SHOCK-WAVE UNDER LORENTZ FORCE AND ENERGY EXCHANGE 16. CHARACTERISTICS OF SHOCK-WAVE UNDER LORENTZ FORCE AND ENERGY EXCHANGE H. Yamasaki, M. Abe and Y. Okuno Graduate School at Nagatsuta, Tokyo Institute of Technology 459, Nagatsuta, Midori-ku, Yokohama,

More information

CHAPTER 16. Basic Concepts. Basic Concepts. The Equilibrium Constant. Reaction Quotient & Equilibrium Constant. Chemical Equilibrium

CHAPTER 16. Basic Concepts. Basic Concepts. The Equilibrium Constant. Reaction Quotient & Equilibrium Constant. Chemical Equilibrium Proerties of an Equilibrium System CHAPTER 6 Chemial Equilibrium Equilibrium systems are DYNAMIC (in onstant motion) REVERSIBLE an be aroahed from either diretion Pink to blue Co(H O) 6 Cl ---> > Co(H

More information

Keywords: pile, liquefaction, lateral spreading, analysis ABSTRACT

Keywords: pile, liquefaction, lateral spreading, analysis ABSTRACT Key arameters in seudo-static analysis of iles in liquefying sand Misko Cubrinovski Deartment of Civil Engineering, University of Canterbury, Christchurch 814, New Zealand Keywords: ile, liquefaction,

More information

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

Chapter 2 Solutions. 2.1 (D) Pressure and temperature are dependent during phase change and independent when in a single phase. Chater Solutions.1 (D) Pressure and temerature are deendent during hase change and indeendent when in a single hase.. (B) Sublimation is the direct conversion of a solid to a gas. To observe this rocess,

More information

whether a process will be spontaneous, it is necessary to know the entropy change in both the

whether a process will be spontaneous, it is necessary to know the entropy change in both the 93 Lecture 16 he entroy is a lovely function because it is all we need to know in order to redict whether a rocess will be sontaneous. However, it is often inconvenient to use, because to redict whether

More information

This relationship is known as the ideal gas law and is mathematically described with the formula below:

This relationship is known as the ideal gas law and is mathematically described with the formula below: Chemistry 20 Ideal as law If we combine all the information contained in Boyle s, Charles and Avoadro s laws, we can derive an expression that describes the temperature, pressure and volume of a as. This

More information

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

AT 25 C! CH10090 Thermodynamics (part 2) Enthalpy changes during reactions. Let s remember what we did in CH10089 CH10090 hermodynamics (art ) Let s remember what we did in CH10089 Enthaly changes during reactions o o o H98 ( reaction) = νi Hf, 98( roducts) νi Hf, 98( reactants) ν i reresents the stoichiometric coefficient.

More information

Week 8 lectures. ρ t +u ρ+ρ u = 0. where µ and λ are viscosity and second viscosity coefficients, respectively and S is the strain tensor:

Week 8 lectures. ρ t +u ρ+ρ u = 0. where µ and λ are viscosity and second viscosity coefficients, respectively and S is the strain tensor: Week 8 lectures. Equations for motion of fluid without incomressible assumtions Recall from week notes, the equations for conservation of mass and momentum, derived generally without any incomressibility

More information

Actual exergy intake to perform the same task

Actual exergy intake to perform the same task CHAPER : PRINCIPLES OF ENERGY CONSERVAION INRODUCION Energy conservation rinciles are based on thermodynamics If we look into the simle and most direct statement of the first law of thermodynamics, we

More information

1 atm = 1.01x10 Pa = 760 Torr = 14.7 lb / in

1 atm = 1.01x10 Pa = 760 Torr = 14.7 lb / in Last class we began discussion of ressure in fluids, with ressure defined as, F = ; units N 1 Pa = 1 m 2 There are a number of other ressure units in common use having the following equivalence, 5 2 1

More information

Research of power plant parameter based on the Principal Component Analysis method

Research of power plant parameter based on the Principal Component Analysis method Research of ower lant arameter based on the Princial Comonent Analysis method Yang Yang *a, Di Zhang b a b School of Engineering, Bohai University, Liaoning Jinzhou, 3; Liaoning Datang international Jinzhou

More information

Lecture 1.2 Units, Dimensions, Estimations 1. Units To measure a quantity in physics means to compare it with a standard. Since there are many

Lecture 1.2 Units, Dimensions, Estimations 1. Units To measure a quantity in physics means to compare it with a standard. Since there are many Lecture. Units, Dimensions, Estimations. Units To measure a quantity in hysics means to comare it with a standard. Since there are many different quantities in nature, it should be many standards for those

More information

Flow Velocity Measurement Principles of Hot Film Anemometry

Flow Velocity Measurement Principles of Hot Film Anemometry Flow Velocity Measurement Princiles of Hot Film Anemometry The hot film anemometer (HFA) is made of a thin, structured, metallic resistive film ( heater ) which is deosited onto a substrate. In the oerating

More information

2.6 Primitive equations and vertical coordinates

2.6 Primitive equations and vertical coordinates Chater 2. The continuous equations 2.6 Primitive equations and vertical coordinates As Charney (1951) foresaw, most NWP modelers went back to using the rimitive equations, with the hydrostatic aroximation,

More information

Synoptic Meteorology I: The Geostrophic Approximation. 30 September, 7 October 2014

Synoptic Meteorology I: The Geostrophic Approximation. 30 September, 7 October 2014 The Equations of Motion Synotic Meteorology I: The Geostrohic Aroimation 30 Setember, 7 October 2014 In their most general form, and resented without formal derivation, the equations of motion alicable

More information

Chapter 5 Mass, Momentum, and Energy Equations

Chapter 5 Mass, Momentum, and Energy Equations 57:00 Mechanics of Fluids and Transort Processes Chater 5 Professor Fred Stern Fall 006 Chater 5 Mass, Momentum, and Energy Equations Flow Rate and Conservation of Mass. cross-sectional area oriented normal

More information

5 Shallow water Q-G theory.

5 Shallow water Q-G theory. 5 Shallow water Q-G theory. So far we have discussed the fact that lare scale motions in the extra-tropical atmosphere are close to eostrophic balance i.e. the Rossby number is small. We have examined

More information

Hypersonic flow: introduction

Hypersonic flow: introduction Hyersonic flow: introduction Van Dyke: Hyersonic flow is flow ast a body at high ach number, where nonlinearity is an essential feature of the flow. Also understood, for thin bodies, that if is the thickness-to-chord

More information

Measurement of cyclone separator

Measurement of cyclone separator Measurement of cyclone searator. Aim of the measurement Cyclones are widely used in industry (in food and chemical industry, in energy technology and in buildings) to remove dust and other articles from

More information

Sedimentation. Treatment Processes. Sedimentation. Sedimentation. Sedimentation. Sedimentation. CIVL 1112 Water Treatment - Sedimentation 1/7

Sedimentation. Treatment Processes. Sedimentation. Sedimentation. Sedimentation. Sedimentation. CIVL 1112 Water Treatment - Sedimentation 1/7 CIVL 111 Water Treatment - 1/7 Treatment Processes is te donards movement of an object relative to its surrounding medium, due to te force of gravity. Screening Aeration Preclorination locculation Coagulation

More information

Understanding and Using Availability

Understanding and Using Availability Understanding and Using Availability Jorge Luis Romeu, Ph.D. ASQ CQE/CRE, & Senior Member Email: romeu@cortland.edu htt://myrofile.cos.com/romeu ASQ/RD Webinar Series Noviembre 5, J. L. Romeu - Consultant

More information

Steven Burian Civil & Environmental Engineering September 25, 2013

Steven Burian Civil & Environmental Engineering September 25, 2013 Fundamentals of Engineering (FE) Exam Mechanics Steven Burian Civil & Environmental Engineering September 25, 2013 s and FE Morning ( Mechanics) A. Flow measurement 7% of FE Morning B. properties Session

More information

12.808: Some Physical Properties of Sea Water or, More than you ever wanted to know about the basic state variables of the ocean

12.808: Some Physical Properties of Sea Water or, More than you ever wanted to know about the basic state variables of the ocean 12.88: Some Physical Proerties of Sea Water or, More than you ever wanted to know about the basic state variables of the ocean Salinity Various salt constituents in 1 m 3 of seawater having (t, S) = (2,

More information

What is Physical Chemistry?

What is Physical Chemistry? Chemistry 313 Dr. Caleb Arrington 10:30 am - 11:20 am M,W,&F Lab: Wednesday 2:00-5:00 Office RMSC 306-A What do we do the first day of every class? syllabus What is Physical Chemistry? Mathematically redictive

More information

Lecture 8, the outline

Lecture 8, the outline Lecture, the outline loose end: Debye theory of solids more remarks on the first order hase transition. Bose Einstein condensation as a first order hase transition 4He as Bose Einstein liquid Lecturer:

More information

Material Balance Method

Material Balance Method Material alance Method Dr. Mahbubur Rahman Deartment of Petroleum & Mineral Resources Enineerin anladesh University of Enineerin & Technoloy Short Course on Petroleum Reserve Estimation, Production and

More information

First law of thermodynamics (Jan 12, 2016) page 1/7. Here are some comments on the material in Thompkins Chapter 1

First law of thermodynamics (Jan 12, 2016) page 1/7. Here are some comments on the material in Thompkins Chapter 1 First law of thermodynamics (Jan 12, 2016) age 1/7 Here are some comments on the material in Thomkins Chater 1 1) Conservation of energy Adrian Thomkins (eq. 1.9) writes the first law as: du = d q d w

More information

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

Unit code: H/ QCF level: 5 Credit value: 15 OUTCOME 1 - THERMODYNAMIC SYSTEMS TUTORIAL 2 Unit 43: Plant and Process Princiles Unit code: H/60 44 QCF level: 5 Credit value: 5 OUCOME - HERMODYNAMIC SYSEMS UORIAL Understand thermodynamic systems as alied to lant engineering rocesses hermodynamic

More information

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

I have not proofread these notes; so please watch out for typos, anything misleading or just plain wrong. hermodynamics I have not roofread these notes; so lease watch out for tyos, anything misleading or just lain wrong. Please read ages 227 246 in Chater 8 of Kittel and Kroemer and ay attention to the first

More information

REVIEW & SUMMARY. Molar Specific Heats The molar specific heat C V of a gas at constant volume is defined as

REVIEW & SUMMARY. Molar Specific Heats The molar specific heat C V of a gas at constant volume is defined as REIEW & SUMMARY 59 PART Kinetic Theory of Gases The kinetic theory of gases relates the macroscoic roerties of gases (for examle, ressure and temerature) to the microscoic roerties of gas molecules (for

More information

Phase Equilibrium Calculations by Equation of State v2

Phase Equilibrium Calculations by Equation of State v2 Bulletin of Research Center for Comuting and Multimedia Studies, Hosei University, 7 (3) Published online (htt://hdl.handle.net/4/89) Phase Equilibrium Calculations by Equation of State v Yosuke KATAOKA

More information

Statics and dynamics: some elementary concepts

Statics and dynamics: some elementary concepts 1 Statics and dynamics: some elementary concets Dynamics is the study of the movement through time of variables such as heartbeat, temerature, secies oulation, voltage, roduction, emloyment, rices and

More information

International Journal of Mathematics Trends and Technology- Volume3 Issue4-2012

International Journal of Mathematics Trends and Technology- Volume3 Issue4-2012 Effect of Hall current on Unsteady Flow of a Dusty Conducting Fluid through orous medium between Parallel Porous Plates with Temerature Deendent Viscosity and Thermal Radiation Harshbardhan Singh and Dr.

More information

Convective Mass Transfer

Convective Mass Transfer Convective Mass Transfer Definition of convective mass transfer: The transport of material between a boundary surface and a moving fluid or between two immiscible moving fluids separated by a mobile interface

More information

s and FE X. A. Flow measurement B. properties C. statics D. impulse, and momentum equations E. Pipe and other internal flow 7% of FE Morning Session I

s and FE X. A. Flow measurement B. properties C. statics D. impulse, and momentum equations E. Pipe and other internal flow 7% of FE Morning Session I Fundamentals of Engineering (FE) Exam General Section Steven Burian Civil & Environmental Engineering October 26, 2010 s and FE X. A. Flow measurement B. properties C. statics D. impulse, and momentum

More information

Paper C Exact Volume Balance Versus Exact Mass Balance in Compositional Reservoir Simulation

Paper C Exact Volume Balance Versus Exact Mass Balance in Compositional Reservoir Simulation Paer C Exact Volume Balance Versus Exact Mass Balance in Comositional Reservoir Simulation Submitted to Comutational Geosciences, December 2005. Exact Volume Balance Versus Exact Mass Balance in Comositional

More information

We now turn to considerations of mixtures. To keep our discussion reasonably simple,

We now turn to considerations of mixtures. To keep our discussion reasonably simple, 143 Lecture 23 We now turn to considerations of mixtures. To kee our discussion reasonably simle, we will limit our discussion to non-reacting systems, and to non-ionic systems. In other words, we will

More information

Turbulent Flow Simulations through Tarbela Dam Tunnel-2

Turbulent Flow Simulations through Tarbela Dam Tunnel-2 Engineering, 2010, 2, 507-515 doi:10.4236/eng.2010.27067 Published Online July 2010 (htt://www.scirp.org/journal/eng) 507 Turbulent Flow Simulations through Tarbela Dam Tunnel-2 Abstract Muhammad Abid,

More information

Chemistry 531 Spring 2009 Problem Set 6 Solutions

Chemistry 531 Spring 2009 Problem Set 6 Solutions Chemistry 531 Sring 2009 Problem Set 6 Solutions 1. In a thermochemical study of N 2, the following heat caacity data were found: t 0 C,m d 27.2Jmol 1 K 1 f t b f C,m d 23.4Jmol 1 K 1 C,m d 11.4Jmol 1

More information

(a) 1m s -2 (b) 2 m s -2 (c) zero (d) -1 m s -2

(a) 1m s -2 (b) 2 m s -2 (c) zero (d) -1 m s -2 11 th Physics - Unit 2 Kinematics Solutions for the Textbook Problems One Marks 1. Which one of the followin Cartesian coordinate system is not followed in physics? 5. If a particle has neative velocity

More information

THE FIRST LAW OF THERMODYNAMICS

THE FIRST LAW OF THERMODYNAMICS THE FIRST LA OF THERMODYNAMIS 9 9 (a) IDENTIFY and SET UP: The ressure is constant and the volume increases (b) = d Figure 9 Since is constant, = d = ( ) The -diagram is sketched in Figure 9 The roblem

More information

Chapter 8 Internal Forced Convection

Chapter 8 Internal Forced Convection Chater 8 Internal Forced Convection 8.1 Hydrodynamic Considerations 8.1.1 Flow Conditions may be determined exerimentally, as shown in Figs. 7.1-7.2. Re D ρumd μ where u m is the mean fluid velocity over

More information

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

Chapter 20: Exercises: 3, 7, 11, 22, 28, 34 EOC: 40, 43, 46, 58 Chater 0: Exercises:, 7,,, 8, 4 EOC: 40, 4, 46, 8 E: A gasoline engine takes in.80 0 4 and delivers 800 of work er cycle. The heat is obtained by burning gasoline with a heat of combustion of 4.60 0 4.

More information

Principles of Computed Tomography (CT)

Principles of Computed Tomography (CT) Page 298 Princiles of Comuted Tomograhy (CT) The theoretical foundation of CT dates back to Johann Radon, a mathematician from Vienna who derived a method in 1907 for rojecting a 2-D object along arallel

More information

1 such that v k g. v g. u g

1 such that v k g. v g. u g Mesoscale Meteoroloy: Quasi-Geostrohic Theory 4, 6 February 7 Wait this is a mesoscale class why do we care about a tenet o synotic meteoroloy?? On the synotic-scale, scale analysis o the orcin terms in

More information

Phone: , For Educational Use. SOFTbank E-Book Center, Tehran. Fundamentals of Heat Transfer. René Reyes Mazzoco

Phone: , For Educational Use. SOFTbank E-Book Center, Tehran. Fundamentals of Heat Transfer. René Reyes Mazzoco 8 Fundamentals of Heat Transfer René Reyes Mazzoco Universidad de las Américas Puebla, Cholula, Mexico 1 HEAT TRANSFER MECHANISMS 1.1 Conduction Conduction heat transfer is explained through the molecular

More information

Analysis of a pneumatic system for a two-phase flow sugar

Analysis of a pneumatic system for a two-phase flow sugar Int. Jnl. of Multihysics Volume 7 Number 4 2013 325 Analysis of a neumatic system for a two-hase flow suar Gustavo J. Otero R. 1, Geanette Polanco 2 and Miuel Asuaje 3 1 Universidad Simón Bolívar, Laboratorio

More information

u y

u y VO., NO., FEBRUARY 8 ISSN 89-668 6-8 Asian Research Publishing Network (ARPN). All rights reserved. NON-NEWTONIAN EFFECTS OF OAD CARRYING CAPACITY AND FRICTIONA FORCE USING RABINOWITS FUID ON TE PERFORMANCE

More information