Viktor Shkolnikov, Juan G. Santiago*

Size: px
Start display at page:

Download "Viktor Shkolnikov, Juan G. Santiago*"

Transcription

1 Supplementar Information: Coupling Isotachophoresis with Affinit Chromatograph for Rapid and Selective Purification with High Column Utilization. Part I: Theor Viktor Shkolnikov, Juan G. Santiago* Department of Mechanical Engineering, Stanford Universit, Stanford, CA 9435, USA. * Tel: ; Fa: ; juan.santiago@stanford.edu In this supplementar information document, we present additional information on the following topic: SI. Solution to the simplified advection-reaction equations SI. Separation resolution of ITP-AC

2 SI. Solution to the simplified advection-reaction equations We solve the simplified advection-reaction equations derived in Section. of the main tet. We start b finding the zeroth order solution for c and n following Thomas but using the boundar and initial conditions pertinent to our problem. We then follow a similar procedure to find first and second order solutions. Similar procedure can be applied to obtain higher order solutions. However, in the main tet we discuss and eplain the trends given onl b the zeroth order solution (accurate to O( ε ) ), as it is the simplest engineering approimation to this problem. Fortunatel, the results of the zeroth order solution agree well with eperimental measurements of ke ITP-AC parameters at our eperimental conditions (presented in Part II of this two-paper 3 series). At the end of this section we present the solution accurate to O( ε ) for situations where knowledge of spatiotemporal behavior of ITP-AC is needed to greater accurac. While we continue to work with the non-dimensionalized equations (as we have in Section. of the main tet), we here drop the asterisks above the variables for clarit of presentation. SI. Solution of zeroth order equations We begin b transforming the two zeroth order equations into a coordinate moving with the LE- TE interface velocit (for the non-dimensionalized equations this velocit equals to unit). We then convert the result into a potential function form, thereb collapsing the two equations into a single equation. We then solve the resulting equation using Laplace transforms. We write the zeroth order non-dimensionalized equations and their respective boundar and initial conditions here again for convenience: c c n t z t + + =, () n t c n + n =, c n ( z ) ( z ), =,, =, () (3) = ( ) c, t α π ep t Da 3. (4) We begin b transforming () through (4) into new independent variables, = z and = ( t z) : c n + =, (5)

3 n c n + n =, c n ( ) ( ), =,, =, (6) (7) = ( ) c, α π ep Da 3. (8) Net we introduce a potential function f such that n c =, (9) =. The potential function f automaticall satisfies equation (5). Therefore, we substitute (9) into (6) and obtain f + + =. () Equation () is non-linear and we linearize it b substituting in after which we obtain φ f, = + ln,, () φ = φ. () In this wa, we have condensed equations (5) and (6) into a single equation (). Net we transform the initial and the boundar conditions. We note that we use the onl initial condition for c. The initial condition on n was applied much earlier, when we tacitl assumed that there is no bound target initiall in the affinit region. See the main tet when we first introduce the reaction equation in terms of N (eq. () of main tet). The transformed initial and boundar conditions are φ (,) = = c(, ), φ (,) (3) 3

4 φ (, ) = = + c(, ). φ (, ) (4) We solve the differential equations (3) and (4) and obtain φ, ep ', ', (5) ( ) = c( ) d = H φ(, ) = ep + c(, ' ) d ' = G( ). (6) Net we appl the Laplace transform to equation () and use the result (6) to obtain, dφ dh p = φ+ (7) d d φ is where the overbar denotes the Laplace transform of a function with respect to (e.g., (, p) the Laplace transform of φ and p is the Laplace transform variable). Also, ( p) G( p) φ, =. (8) We solve the differential equation (7) b variation of parameters to obtain ( ') ( ') (, ) dh φ p = G p ep ep d'. p + p (9) d p We then take the inverse transform of (9) to obtain where ( ') φ, = G ' F, ' d ' + dh F ', d ', d () L F L F, = ep, p ( ), ep. p p ( ) = () L F, F,. Taking the inverse Laplace transform of () we obtain 4 designates the Laplace transform of

5 F(, ) = I( ) + δ( ), = ( ) F, I. () Here I and I are modified Bessel functions of the first kind of zeroth and first order respectivel. We substitute () into () and obtain ( ') ' d dh φ, = G + G ' I ' d ' + I ' d '. (3) We then simplif (3) b evaluating the right hand side term via integration b parts and noticing that G = ( ') ( ') d d φ dg dh, = I + I ' d ' + I ' d '. (4) This is the general solution to the zeroth order equations in terms of the potential function φ. Net we appl the initial and boundar conditions specific to ITP-AC. We begin b substituting (7) into (5) and obtain and Substituting, this simplifies (4) to H dh ( ' ) d = ep, (5) = ep. (6) dg φ, = I + I ' d ' + ep ' I ' d'. (7) d We net appl the boundar condition b substituting (8) into (6) and obtain G αda Da 3 3 = ep + erf erf, (8) and 5

6 α dg Da 3 αda Da 3 3 = ep + ep + erf erf. d π (9) Therefore ( ') dg φ, = I + I ' d ' + ep ' I ' d ', (3) d where dg d is given b (9). Now c and n can be easil obtained b substituting (3) into () and substituting the result into (9). For convenience, we evaluated solutions numericall using custom MATLAB scripts as we analzed the spatiotemporal behavior of the target in ITP- AC. SI. Solution of first order equations We solve the first order equations following a procedure similar to the zeroth order equations. We again begin b transforming the two first order equations into a coordinate moving with the LE-TE interface velocit. We then convert the result into a potential function form, thereb again collapsing the two equations into a single equation. We again solve the resulting equation using Laplace transforms. We write the first order non-dimensionalized equations and their respective boundar and initial conditions here again for convenience: ( uc % ) c c n t z t z =, n t c n c + n =, ( z ) ( z ), =,, =, (3) (3) (33) c(, t ) =. (34) We then transform (3) through (34) into new independent variables, = z and = ( t z) : ( uc % ) ( uc % ) c n + + =, (35) 6

7 n c + n =. (36) Net we define new variables C = c + uc %, M = n uc %, (37) and recast (35) and (36) in these variables: C M + =, (38) M ( uc % ) ( C uc ) ( M uc ) =. % % (39) We also recast the initial and boundar condition in these variables % % C z, u z, c z, =, M z, + u z, c z, =, (4) C, t u%, t c, t =. (4) Net we introduce a potential function f such that M= (4) C = and substitute this into (38) and (39). The potential function f automaticall satisfies equation (38), and (39) becomes ( uc % ) f ( + ) uc = Now we appl f to the initial and boundar conditions ( ) = M ( ) = n ( ) u( ) c ( ) %. (43),,, %,,, (44) 7

8 We integrate (44) and (45) Noticing that n ( ',) = and ( ) = C ( ) = c ( ) u( ) c ( ),,, %,,. (45) % (46) = f, n ', u ', c ', d ', % (47) = f, c, ' u, ' c, ' d '. c, ' = we simplif the above equations to % (48) = = f, u ', c ', d ' H, % (49) = = f, u, ' c, ' d ' G. Equations for initial and boundar conditions (48) and (49) are to be evaluated using the result from the zeroth order equations. u% is of the form of an error function (see main tet), i.e., u % = erf t z 3Da Da. Net, we take the Laplace transform of (43) to ield f p H + f = + H ( + + p) w + w(, ), p+ p+ (5) where w= uc %. We solve differential equation (5) using variation of parameters and obtain f G p p p+ = ep ( ') H p ' p ep ep H( ') ( p) w w( ',) d '. p+ p+ p+ (5) We epand this to ( ' ) H f = G( p) F + + H( ' ) + w( ', ) F d' F3 wd ', (5) 8

9 where p F = ep, p+ F p ' = ep, p+ p+ ( p) p( ' ) + + F3 = ep. p+ p+ (53) We recommend finding the inverse Laplace transforms of equations in (53) numericall. We then take the inverse Laplace transform of (5) to obtain f = G ' F, ' d ' ( ') H H ( ' ) w( ', ) F ( ', ) d ' ( ) w ', ' F, ' d ' d '. 3 (54) Now the functions c and n can be obtained fairl easil b substituting (54) into (4), and using the appropriate inverse Laplace transforms for (53) and the result from the zeroth order equations (as inputs for G, H, and w). We recommend evaluating this numericall using MATLAB. SI.3 Solution of second order equations We solve the second order equations following a similar procedure to the zeroth and first order equations. We once again begin b transforming the two first order equations into a coordinate moving with the LE-TE interface velocit. We then convert the result into a potential function form, again collapsing the two equations into a single equation. We then solve the resulting equation using Laplace transforms. We write the second order non-dimensionalized equations and their respective boundar and initial conditions here again for convenience: ( uc % ) c c n t z t z =, (55) n t c + n + c n =, (56) 9

10 c n ( z ) ( z ), =,, =, (57) c(, t ) =. (58) We transform (55) through (58) into new independent variables, = z and = ( t z) : ( uc % ) ( uc % ) c n + + =, (59) n c + n + c n =. (6) Net, we define new variables C = c + uc %, M = n uc %, (6) and recast (59) and (6) in these variables C M + =, (6) M ( uc % ) + C uc + M + uc + cn =. % % (63) We also recast the initial and boundar condition in these variables % % C z, u z, c z, =, M z, + u z, c z, =, (64) C, t u%, t c, t =. (65) Net we introduce a potential function f such that M =, (66) C =,

11 and substitute this into (6) and (63). The potential function f automaticall satisfies equation (6), and (63) becomes ( uc % ) f ( + ) uc + cn = Now we appl f to the initial and boundar conditions and obtain We integrate (68) and (69) and obtain Noticing that n ( ',) = and ( ) = M ( ) = n ( ) u( ) c ( ) %. (67),,, %,,, (68) ( ) = C ( ) = c ( ) u( ) c ( ),,, %,,. (69) % (7) = f, n ', u ', c ', d ', % (7) = f, c, ' u, ' c, ' d '. c, ' =, we simplif the equations above to % (7) = = f, u ', c ', d ' H, % (73) = = f, u, ' c, ' d ' G. Equations for initial and boundar conditions (7) and (73) are to be evaluated using the result from the first order equations. Net, we take the Laplace transform of (67) to obtain f p H + f = + H ( + + p) w + w(, ) w, p+ p+ (74) where w = uc %, w = nc. We solve differential equation (74) using variation of parameters and obtain

12 ( ) p f = G p +Θ ep, p+ (75) where ( ') ' p H Θ= ep H ( ') ( p) w w( ',) w d '. p (76) + p+ We epand (75) to where ( ' ) H f = G( p) F + + H( ' ) + w( ', ) F d' F3 wd ' + F4 wd ', (77) p F = ep, p+ F 4 p ' = ep, p+ p+ ( p) p( ' ) + + F3 = ep, p+ p+ F ( ' ) p = ep. p+ p+ (78) We then take the inverse Laplace transform of (78) to obtain f = G ' F, ' d ' ( ') H H ( ') w ( ',) F ( ', ) d ' ( ) w ', ' F, ' d ' d' 3 + w ', ' F, ' d ' d '. 4 (79)

13 Now functions c and n can be obtained b substituting (79) into (66) using the appropriate inverse Laplace transforms for (78) and the result from the first order equations (as inputs for G, H, w, and w ). Again, we recommend evaluating this numericall using MATLAB. SI.4 Third order accurate solutions Finall, a third order accurate solution is obtained b combining results obtained from (3), (54), and (79) into where once again, ε is defined as c= c + εc + ε c + O ( ε ), ( ε ) 3 n= n + εn + ε n + O 3 ε µ µ, (8) a, TE TEion, TE =. (8) µ TEion, TE Higher order equations can be obtained in a manner similar to that for first and second order equations and hence even higher order of accurac solutions can be obtained. 3

14 SI. Separation resolution of ITP-AC As described in the main tet, the ideal case for ITP-AC separation is that cn target (where subscript cn refers to contaminant). That is, target should be captured approimatel irreversibl while contaminant is removed and transported downstream. For this regime, the target is captured in time p t while contaminants migrate through the column. We present an eperimental demonstration of such separation in the main tet of Part II of this two-part series. We consider here a regime where the target is completel captured (e.g., 6 < ) while the contaminant species remains focused in ITP and migrating at the ITP velocit. For this regime, we define a simple criterion for the time required to achieve sufficient separation between captured target and contaminant. We appl a common definition of resolution, R, given b Giddings 3 as follows: L R=, σ + σ (8) where L is the distance between the two peaks and, σ and σ are the corresponding standard deviations of the two peaks. We let σ be the standard deviation width of the captured (immobile) target peak and σ the standard deviation of the contaminant peak. In ITP-AC the target attains zero velocit at time approimatel p t, and thereafter the width of the target distribution scales as p z. After the target attains zero velocit, the distance between the target and the analte simpl scales as ut. Using the scaling for the ITP peak width from MacInnes and Longsworth 4,5, we obtain the scaling for resolution for ITP-AC, as we did in equation (4) of the main tet. We write it here again for convenience: R ITP-AC ut u µ L in LEµ T in TE kbt p z * + kn u µ L in LE µ T in TE e, (83) where again, k B is the Boltzmann's constant, T is the absolute temperature, e is the electron charge, and µ L in LE and µ T in TE are the mobilities of the LE ion in the LE and the TE ion in the TE respectivel. We note that the resolution for ITP-AC scales as t. This is in contrast to the resolution of traditional electrophoresis or of AC which scale as t. 6 The resolution of ITP-AC increases with increasing ITP velocit u and it asmptotes to a value of tk N p z * for large u. We can achieve 95% of this resolution with u µ L in LEµ T in TE kbt kn..5 µ L in LE µ T in TE e pz * (84) 4

15 Operating at ITP velocit lower than u 95 results in loss of resolution. Operating at a velocit much higher than u 95 leads to larger capture lengths with little gain in resolution and therefore loss in column utilization (see Section 3.. of the main tet). For a good compromise between resolution and column utilization, we therefore recommend operating at around u 95. For an ITP velocit of u 95 and a convenient resolution, target and contaminant zone), the time to capture and purif, c, p If α Da is also less than unit, then, R ITP-AC, value of, sa, (for well separated capture t is approimatel c p p k N. t is approimatel * 8 k N. For tpical ITP-AC conditions such as those we emploed in Part II of this two-paper series (µ L in LE -6-9 m V - s -, µ T in LE - -9 m V - s -, k = 3 M - s -, N 3 µm, and p z *.8), u95 is on the order of. mm/s and t c, p is approimatel 5 min. 7 z References () Thomas, H. C. J. Am. Chem. Soc. 944, 66, () Wolfram Alpha. Wolfram Alpha LLC, 3. (3) Giddings, J. C. Sep. Sci. Technol. 969, 4, (4) MacInnes, D. A.; Longsworth, L. G. Chem. Rev. 93, 9, 7-3. (5) Shkolnikov, V.; Bahga, S. S.; Santiago, J. G. PCCP, 4, (6) Landers, J. P. Handbook of capillar electrophoresis; CRC press, 997. (7) Shkolnikov, V.; Santiago, J. G. Anal. Chem. 4, submitted. 5

Simultaneous Orthogonal Rotations Angle

Simultaneous Orthogonal Rotations Angle ELEKTROTEHNIŠKI VESTNIK 8(1-2): -11, 2011 ENGLISH EDITION Simultaneous Orthogonal Rotations Angle Sašo Tomažič 1, Sara Stančin 2 Facult of Electrical Engineering, Universit of Ljubljana 1 E-mail: saso.tomaic@fe.uni-lj.si

More information

UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD

UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference Jul 8-23, 999, San Francisco, California FEDSM99-8 UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX

More information

AE/ME 339. K. M. Isaac Professor of Aerospace Engineering. December 21, 2001 topic13_grid_generation 1

AE/ME 339. K. M. Isaac Professor of Aerospace Engineering. December 21, 2001 topic13_grid_generation 1 AE/ME 339 Professor of Aerospace Engineering December 21, 2001 topic13_grid_generation 1 The basic idea behind grid generation is the creation of the transformation laws between the phsical space and the

More information

Properties of Limits

Properties of Limits 33460_003qd //04 :3 PM Page 59 SECTION 3 Evaluating Limits Analticall 59 Section 3 Evaluating Limits Analticall Evaluate a it using properties of its Develop and use a strateg for finding its Evaluate

More information

5.6. Differential equations

5.6. Differential equations 5.6. Differential equations The relationship between cause and effect in phsical phenomena can often be formulated using differential equations which describe how a phsical measure () and its derivative

More information

2.2 SEPARABLE VARIABLES

2.2 SEPARABLE VARIABLES 44 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 6 Consider the autonomous DE 6 Use our ideas from Problem 5 to find intervals on the -ais for which solution curves are concave up and intervals for which

More information

Spotlight on the Extended Method of Frobenius

Spotlight on the Extended Method of Frobenius 113 Spotlight on the Extended Method of Frobenius See Sections 11.1 and 11.2 for the model of an aging spring. Reference: Section 11.4 and SPOTLIGHT ON BESSEL FUNCTIONS. Bessel functions of the first kind

More information

2.3 The Fixed-Point Algorithm

2.3 The Fixed-Point Algorithm .3 The Fied-Point Algorithm 1. Mean Value Theorem: Theorem Rolle stheorem: Suppose that f is continuous on a, b and is differentiable on a, b. If f a f b, then there eists a number c in a, b such that

More information

*

* Quasi-Static Magnetic Field Shielding Using Longitudinal Mu-Near-Zero Metamaterials Gu Lipworth 1, Joshua Ensworth 2, Kushal Seetharam 1, Jae Seung Lee 3, Paul Schmalenberg 3, Tsuoshi Nomura 4, Matthew

More information

Electronic Supplementary Information Increasing Hybridization Rate and Sensitivity of DNA Microarrays Using Isotachophoresis

Electronic Supplementary Information Increasing Hybridization Rate and Sensitivity of DNA Microarrays Using Isotachophoresis Electronic Supplementary Material (ESI) for Lab on a Chip. This journal is The Royal Society of Chemistry 2014 Electronic Supplementary Information Increasing Hybridization Rate and Sensitivity of DNA

More information

Perturbation Theory for Variational Inference

Perturbation Theory for Variational Inference Perturbation heor for Variational Inference Manfred Opper U Berlin Marco Fraccaro echnical Universit of Denmark Ulrich Paquet Apple Ale Susemihl U Berlin Ole Winther echnical Universit of Denmark Abstract

More information

Generalized Least-Squares Regressions III: Further Theory and Classication

Generalized Least-Squares Regressions III: Further Theory and Classication Generalized Least-Squares Regressions III: Further Theor Classication NATANIEL GREENE Department of Mathematics Computer Science Kingsborough Communit College, CUNY Oriental Boulevard, Brookln, NY UNITED

More information

Project 6.2 Phase Plane Portraits of Almost Linear Systems

Project 6.2 Phase Plane Portraits of Almost Linear Systems Project 6.2 Phase Plane Portraits of Almost Linear Sstems Interesting and complicated phase portraits often result from simple nonlinear perturbations of linear sstems. For instance, the figure below shows

More information

10.2 The Unit Circle: Cosine and Sine

10.2 The Unit Circle: Cosine and Sine 0. The Unit Circle: Cosine and Sine 77 0. The Unit Circle: Cosine and Sine In Section 0.., we introduced circular motion and derived a formula which describes the linear velocit of an object moving on

More information

CONTINUOUS SPATIAL DATA ANALYSIS

CONTINUOUS SPATIAL DATA ANALYSIS CONTINUOUS SPATIAL DATA ANALSIS 1. Overview of Spatial Stochastic Processes The ke difference between continuous spatial data and point patterns is that there is now assumed to be a meaningful value, s

More information

SEPARABLE EQUATIONS 2.2

SEPARABLE EQUATIONS 2.2 46 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 4. Chemical Reactions When certain kinds of chemicals are combined, the rate at which the new compound is formed is modeled b the autonomous differential equation

More information

Research Article Development of a Particle Interaction Kernel Function in MPS Method for Simulating Incompressible Free Surface Flow

Research Article Development of a Particle Interaction Kernel Function in MPS Method for Simulating Incompressible Free Surface Flow Journal of Applied Mathematics Volume 2, Article ID 793653, 6 pages doi:.55/2/793653 Research Article Development of a Particle Interaction Kernel Function in MPS Method for Simulating Incompressible Free

More information

Quiz #2. A = 1 2 bh 1 2 (6.1)(5.3)

Quiz #2. A = 1 2 bh 1 2 (6.1)(5.3) Math 50C Multivariable Calculus September 11, 2015 Quiz #2 Name: Answer Ke David Arnold Instructions. (20 points) This quiz is open notes, open book. This includes an supplementar tets or online documents.

More information

8.1 Exponents and Roots

8.1 Exponents and Roots Section 8. Eponents and Roots 75 8. Eponents and Roots Before defining the net famil of functions, the eponential functions, we will need to discuss eponent notation in detail. As we shall see, eponents

More information

5.3.3 The general solution for plane waves incident on a layered halfspace. The general solution to the Helmholz equation in rectangular coordinates

5.3.3 The general solution for plane waves incident on a layered halfspace. The general solution to the Helmholz equation in rectangular coordinates 5.3.3 The general solution for plane waves incident on a laered halfspace The general solution to the elmhol equation in rectangular coordinates The vector propagation constant Vector relationships between

More information

6 = 1 2. The right endpoints of the subintervals are then 2 5, 3, 7 2, 4, 2 9, 5, while the left endpoints are 2, 5 2, 3, 7 2, 4, 9 2.

6 = 1 2. The right endpoints of the subintervals are then 2 5, 3, 7 2, 4, 2 9, 5, while the left endpoints are 2, 5 2, 3, 7 2, 4, 9 2. 5 THE ITEGRAL 5. Approimating and Computing Area Preliminar Questions. What are the right and left endpoints if [, 5] is divided into si subintervals? If the interval [, 5] is divided into si subintervals,

More information

EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING

EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING A Thesis b BRENT DURRELL PICKLE Submitted to the Office of Graduate Studies of Teas A&M Universit in partial fulfillment

More information

The Control-Volume Finite-Difference Approximation to the Diffusion Equation

The Control-Volume Finite-Difference Approximation to the Diffusion Equation The Control-Volume Finite-Difference Approimation to the Diffusion Equation ME 448/548 Notes Gerald Recktenwald Portland State Universit Department of Mechanical Engineering gerr@mepdedu ME 448/548: D

More information

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin.

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin. THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY 1. Introduction V. A. Sharifulin Perm State Technical Universit, Perm, Russia e-mail: sharifulin@perm.ru Water

More information

ME615 Project Report Aeroacoustic Simulations using Lattice Boltzmann Method

ME615 Project Report Aeroacoustic Simulations using Lattice Boltzmann Method ME615 Project Report Aeroacoustic Simulations using Lattice Boltzmann Method Kameswararao Anupindi School of Mechanical Engineering, Purdue Universit, West Lafaette, IN, 4796, USA Lattice Boltzmann method

More information

Heat Conduction in semi-infinite Slab

Heat Conduction in semi-infinite Slab 1 Module : Diffusive heat and mass transfer Lecture 11: Heat Conduction in semi-infinite Slab with Constant wall Temperature Semi-infinite Solid Semi-infinite solids can be visualized as ver thick walls

More information

Multivariable Calculus Lecture #13 Notes. in each piece. Then the mass mk. 0 σ = σ = σ

Multivariable Calculus Lecture #13 Notes. in each piece. Then the mass mk. 0 σ = σ = σ Multivariable Calculus Lecture #1 Notes In this lecture, we ll loo at parameterization of surfaces in R and integration on a parameterized surface Applications will include surface area, mass of a surface

More information

Apply mass and momentum conservation to a differential control volume. Simple classical solutions of NS equations

Apply mass and momentum conservation to a differential control volume. Simple classical solutions of NS equations Module 5: Navier-Stokes Equations: Appl mass and momentum conservation to a differential control volume Derive the Navier-Stokes equations Simple classical solutions of NS equations Use dimensional analsis

More information

MATHEMATICS 200 December 2014 Final Exam Solutions

MATHEMATICS 200 December 2014 Final Exam Solutions MATHEMATICS 2 December 214 Final Eam Solutions 1. Suppose that f,, z) is a function of three variables and let u 1 6 1, 1, 2 and v 1 3 1, 1, 1 and w 1 3 1, 1, 1. Suppose that at a point a, b, c), Find

More information

4 Inverse function theorem

4 Inverse function theorem Tel Aviv Universit, 2013/14 Analsis-III,IV 53 4 Inverse function theorem 4a What is the problem................ 53 4b Simple observations before the theorem..... 54 4c The theorem.....................

More information

Two-Dimensional Analysis of the Power Transfer between Crossed Laser Beams

Two-Dimensional Analysis of the Power Transfer between Crossed Laser Beams Two-Dimensional Analsis of the Power Transfer between Crossed Laser Beams The indirect-drive approach to inertial confinement fusion involves laser beams that cross as the enter the hohlraum. Ionacoustic

More information

8.7 Systems of Non-Linear Equations and Inequalities

8.7 Systems of Non-Linear Equations and Inequalities 8.7 Sstems of Non-Linear Equations and Inequalities 67 8.7 Sstems of Non-Linear Equations and Inequalities In this section, we stud sstems of non-linear equations and inequalities. Unlike the sstems of

More information

7. TURBULENCE SPRING 2019

7. TURBULENCE SPRING 2019 7. TRBLENCE SPRING 2019 7.1 What is turbulence? 7.2 Momentum transfer in laminar and turbulent flow 7.3 Turbulence notation 7.4 Effect of turbulence on the mean flow 7.5 Turbulence generation and transport

More information

A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS

A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS 1 A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS An ESIS Protocol Revised June 2007, Nov 2010 D R Moore, J G Williams

More information

Strain Transformation and Rosette Gage Theory

Strain Transformation and Rosette Gage Theory Strain Transformation and Rosette Gage Theor It is often desired to measure the full state of strain on the surface of a part, that is to measure not onl the two etensional strains, and, but also the shear

More information

Joule Heating Effects on MHD Natural Convection Flows in Presence of Pressure Stress Work and Viscous Dissipation from a Horizontal Circular Cylinder

Joule Heating Effects on MHD Natural Convection Flows in Presence of Pressure Stress Work and Viscous Dissipation from a Horizontal Circular Cylinder Journal of Applied Fluid Mechanics, Vol. 7, No., pp. 7-3, 04. Available online at www.jafmonline.net, ISSN 735-357, EISSN 735-3645. Joule Heating Effects on MHD Natural Convection Flows in Presence of

More information

LESSON #48 - INTEGER EXPONENTS COMMON CORE ALGEBRA II

LESSON #48 - INTEGER EXPONENTS COMMON CORE ALGEBRA II LESSON #8 - INTEGER EXPONENTS COMMON CORE ALGEBRA II We just finished our review of linear functions. Linear functions are those that grow b equal differences for equal intervals. In this unit we will

More information

MAXIMA & MINIMA The single-variable definitions and theorems relating to extermals can be extended to apply to multivariable calculus.

MAXIMA & MINIMA The single-variable definitions and theorems relating to extermals can be extended to apply to multivariable calculus. MAXIMA & MINIMA The single-variable definitions and theorems relating to etermals can be etended to appl to multivariable calculus. ( ) is a Relative Maimum if there ( ) such that ( ) f(, for all points

More information

Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators. Abstract

Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators. Abstract Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators Rajendra Singh and Seungbo Kim The Ohio State Universit Columbus, OH 4321-117, USA Abstract Much of the vibration isolation

More information

SIMPLE EXPLICIT EXPRESSIONS FOR CALCULATION OF THE HEISLER-GROBER CHARTS. M.M. Yovanovich. Microelectronics Heat Transfer Laboratory

SIMPLE EXPLICIT EXPRESSIONS FOR CALCULATION OF THE HEISLER-GROBER CHARTS. M.M. Yovanovich. Microelectronics Heat Transfer Laboratory SIMPLE EXPLICIT EXPRESSIONS FOR CALCULATION OF THE HEISLER-GROBER CHARTS M.M. Yovanovich Microelectronics Heat Transfer Laborator Department of Mechanical Engineering Universit ofwaterloo Waterloo Ontario

More information

Supplementary Information Ionic Strength Effects on Electrophoretic Focusing and Separations Supreet S. Bahga, Moran Bercovici, and Juan G.

Supplementary Information Ionic Strength Effects on Electrophoretic Focusing and Separations Supreet S. Bahga, Moran Bercovici, and Juan G. Supplementary Information Ionic Strength Effects on Electrophoretic Focusing and Separations Supreet S. Bahga, Moran Bercovici, and Juan G. Santiago We here present further details on the injection protocol

More information

Theory of Optical Waveguide

Theory of Optical Waveguide Theor of Optical Waveguide Class: Integrated Photonic Devices Time: Fri. 8:am ~ :am. Classroom: 資電 6 Lecturer: Prof. 李明昌 (Ming-Chang Lee Reflection and Refraction at an Interface (TE n kˆi H i E i θ θ

More information

INTRODUCTION TO DIFFERENTIAL EQUATIONS

INTRODUCTION TO DIFFERENTIAL EQUATIONS INTRODUCTION TO DIFFERENTIAL EQUATIONS. Definitions and Terminolog. Initial-Value Problems.3 Differential Equations as Mathematical Models CHAPTER IN REVIEW The words differential and equations certainl

More information

The Gas-assisted Expelled Fluid Flow in the Front of a Long Bubble in a Channel

The Gas-assisted Expelled Fluid Flow in the Front of a Long Bubble in a Channel C. H. Hsu, P. C. Chen,. Y. ung, G. C. uo The Gas-assisted Epelled Fluid Flow in the Front of a Long Bubble in a Channel C.H. Hsu 1, P.C. Chen 3,.Y. ung, and G.C. uo 1 1 Department of Mechanical Engineering

More information

Chapter-2: A Generalized Ratio and Product Type Estimator for the Population Mean in Stratified Random Sampling CHAPTER-2

Chapter-2: A Generalized Ratio and Product Type Estimator for the Population Mean in Stratified Random Sampling CHAPTER-2 Capter-: A Generalized Ratio and Product Tpe Eimator for te Population Mean in tratified Random ampling CHAPTER- A GEERALIZED RATIO AD PRODUCT TYPE ETIMATOR FOR THE POPULATIO MEA I TRATIFIED RADOM AMPLIG.

More information

INTERFACE CRACK IN ORTHOTROPIC KIRCHHOFF PLATES

INTERFACE CRACK IN ORTHOTROPIC KIRCHHOFF PLATES Gépészet Budapest 4-5.Ma. G--Section-o ITERFACE CRACK I ORTHOTROPIC KIRCHHOFF PLATES András Szekrénes Budapest Universit of Technolog and Economics Department of Applied Mechanics Budapest Műegetem rkp.

More information

Experiment 7 Energy Loss in a Hydraulic Jump

Experiment 7 Energy Loss in a Hydraulic Jump Experiment 7 Energ Loss in a Hdraulic Jump n Purpose: The purpose of this experiment is to examine the transition from supercritical (rapid) flow to subcritical (slow) flow in an open channel and to analze

More information

where a 0 and the base b is a positive number other

where a 0 and the base b is a positive number other 7. Graph Eponential growth functions No graphing calculators!!!! EXPONENTIAL FUNCTION A function of the form than one. a b where a 0 and the base b is a positive number other a = b = HA = Horizontal Asmptote:

More information

INF Introduction to classifiction Anne Solberg

INF Introduction to classifiction Anne Solberg INF 4300 8.09.17 Introduction to classifiction Anne Solberg anne@ifi.uio.no Introduction to classification Based on handout from Pattern Recognition b Theodoridis, available after the lecture INF 4300

More information

3.1 Exponential Functions and Their Graphs

3.1 Exponential Functions and Their Graphs .1 Eponential Functions and Their Graphs Sllabus Objective: 9.1 The student will sketch the graph of a eponential, logistic, or logarithmic function. 9. The student will evaluate eponential or logarithmic

More information

Simulation of Acoustic and Vibro-Acoustic Problems in LS-DYNA using Boundary Element Method

Simulation of Acoustic and Vibro-Acoustic Problems in LS-DYNA using Boundary Element Method 10 th International LS-DYNA Users Conference Simulation Technolog (2) Simulation of Acoustic and Vibro-Acoustic Problems in LS-DYNA using Boundar Element Method Yun Huang Livermore Software Technolog Corporation

More information

Stability Of Structures: Continuous Models

Stability Of Structures: Continuous Models 5 Stabilit Of Structures: Continuous Models SEN 311 ecture 5 Slide 1 Objective SEN 311 - Structures This ecture covers continuous models for structural stabilit. Focus is on aiall loaded columns with various

More information

PHASE SPACE TOMOGRAPHY OF BEAMS WITH EXTREME SPACE CHARGE *

PHASE SPACE TOMOGRAPHY OF BEAMS WITH EXTREME SPACE CHARGE * PHASE SPACE TOMOGRAPHY OF BEAMS WITH EXTREME SPACE CHARGE * D. Stratakis #, R. A. Kishek, I. Haber, M. Walter, R. B. Fiorito, S. Bernal, J.C.T. Thangaraj, K. Tian, C. Papadopoulos, M. Reiser, P. G. O Shea

More information

UNIVERSIDAD CARLOS III DE MADRID MATHEMATICS II EXERCISES (SOLUTIONS )

UNIVERSIDAD CARLOS III DE MADRID MATHEMATICS II EXERCISES (SOLUTIONS ) UNIVERSIDAD CARLOS III DE MADRID MATHEMATICS II EXERCISES (SOLUTIONS ) CHAPTER : Limits and continuit of functions in R n. -. Sketch the following subsets of R. Sketch their boundar and the interior. Stud

More information

A Method for Geometry Optimization in a Simple Model of Two-Dimensional Heat Transfer

A Method for Geometry Optimization in a Simple Model of Two-Dimensional Heat Transfer A Method for Geometr Optimization in a Simple Model of Two-Dimensional Heat Transfer X. Peng, K. Niakhai B. Protas Jul, 3 arxiv:37.48v [math.na] 4 Jul 3 Abstract This investigation is motivated b the problem

More information

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Chapter 8 KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Figure 8.1: 195 196 CHAPTER 8. KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS 8.1 Motivation In Chapter 3, the conservation of linear momentum for a

More information

EDEXCEL ANALYTICAL METHODS FOR ENGINEERS H1 UNIT 2 - NQF LEVEL 4 OUTCOME 4 - STATISTICS AND PROBABILITY TUTORIAL 3 LINEAR REGRESSION

EDEXCEL ANALYTICAL METHODS FOR ENGINEERS H1 UNIT 2 - NQF LEVEL 4 OUTCOME 4 - STATISTICS AND PROBABILITY TUTORIAL 3 LINEAR REGRESSION EDEXCEL AALYTICAL METHODS FOR EGIEERS H1 UIT - QF LEVEL 4 OUTCOME 4 - STATISTICS AD PROBABILITY TUTORIAL 3 LIEAR REGRESSIO Tabular and graphical form: data collection methods; histograms; bar charts; line

More information

Two-Dimensional Formulation.

Two-Dimensional Formulation. Two-Dimensional Formulation mi@seu.edu.cn Outline Introduction( 概论 ) Two vs. Three-Dimensional Problems Plane Strain( 平面应变 ) Plane Stress( 平面应力 ) Boundar Conditions( 边界条件 ) Correspondence between Plane

More information

FACULTY OF MATHEMATICAL STUDIES MATHEMATICS FOR PART I ENGINEERING. Lectures AB = BA = I,

FACULTY OF MATHEMATICAL STUDIES MATHEMATICS FOR PART I ENGINEERING. Lectures AB = BA = I, FACULTY OF MATHEMATICAL STUDIES MATHEMATICS FOR PART I ENGINEERING Lectures MODULE 7 MATRICES II Inverse of a matri Sstems of linear equations Solution of sets of linear equations elimination methods 4

More information

arxiv: v1 [nlin.ps] 3 Sep 2009

arxiv: v1 [nlin.ps] 3 Sep 2009 Soliton, kink and antikink solutions o a 2-component o the Degasperis-Procesi equation arxiv:0909.0659v1 [nlin.ps] 3 Sep 2009 Jiangbo Zhou, Liin Tian, Xinghua Fan Nonlinear Scientiic Research Center, Facult

More information

CHAPTER 80 NUMERICAL METHODS FOR FIRST-ORDER DIFFERENTIAL EQUATIONS

CHAPTER 80 NUMERICAL METHODS FOR FIRST-ORDER DIFFERENTIAL EQUATIONS CHAPTER 8 NUMERICAL METHODS FOR FIRST-ORDER DIFFERENTIAL EQUATIONS EXERCISE 33 Page 834. Use Euler s method to obtain a numerical solution of the differential equation d d 3, with the initial conditions

More information

Contact lines on soft solids with uniform surface tension: analytical solutions and double transition for increasing deformability

Contact lines on soft solids with uniform surface tension: analytical solutions and double transition for increasing deformability rspa.roalsocietpublishing.org Research Cite this article: Dervau J, Limat L. 2015 Contact lines on soft solids with uniform surface tension: analticaolutions and double transition for increasing deformabilit.

More information

Chemistry 141 Laboratory Lab Lecture Notes for Kinetics Lab Dr Abrash

Chemistry 141 Laboratory Lab Lecture Notes for Kinetics Lab Dr Abrash Q: What is Kinetics? Chemistr 141 Laborator Lab Lecture Notes for Kinetics Lab Dr Abrash Kinetics is the stud of rates of reaction, i.e., the stud of the factors that control how quickl a reaction occurs.

More information

Limits and Their Properties

Limits and Their Properties Limits and Their Properties The it of a function is the primar concept that distinguishes calculus from algebra and analtic geometr. The notion of a it is fundamental to the stud of calculus. Thus, it

More information

Dynamics of quantum vortices in a toroidal trap

Dynamics of quantum vortices in a toroidal trap PHYSICAL REVIEW A 79, 4362 29 Dnamics of quantum vortices in a toroidal trap Peter Mason and Natalia G. Berloff Department of Applied Mathematics and Theoretical Phsics, Universit of Cambridge, Wilberforce

More information

Derivatives CHAPTER. 3.1 Derivative of a Function. 3.2 Differentiability. 3.3 Rules for Differentiation. 3.4 Velocity and Other Rates of Change

Derivatives CHAPTER. 3.1 Derivative of a Function. 3.2 Differentiability. 3.3 Rules for Differentiation. 3.4 Velocity and Other Rates of Change CHAPTER 3 Derivatives 3. Derivative of a Function 3. Differentiabilit 3.3 Rules for Differentiation 3.4 Velocit and ther Rates of Change 3.5 Derivatives of Trigonometric Functions Shown here is the pain

More information

On the Effect of the Boundary Conditions and the Collision Model on Rarefied Gas Flows

On the Effect of the Boundary Conditions and the Collision Model on Rarefied Gas Flows On the Effect of the Boundar Conditions and the Collision Model on Rarefied Gas Flows M. Vargas a, S. Stefanov a and D. Valougeorgis b a Institute of Mechanics, Bulgarian Academ of Sciences, Acad. G. Bonchev

More information

Ceramic Processing Research

Ceramic Processing Research Journal of Ceramic Processing Research. Vol. 10, No. 2, pp. 195~201 (2009) J O U R N A L O F Ceramic Processing Research Computer simulation of a ceramics powder compaction process and optimization of

More information

Conic Sections CHAPTER OUTLINE. The Circle Ellipses and Hyperbolas Second-Degree Inequalities and Nonlinear Systems FIGURE 1

Conic Sections CHAPTER OUTLINE. The Circle Ellipses and Hyperbolas Second-Degree Inequalities and Nonlinear Systems FIGURE 1 088_0_p676-7 /7/0 :5 PM Page 676 (FPG International / Telegraph Colour Librar) Conic Sections CHAPTER OUTLINE. The Circle. Ellipses and Hperbolas.3 Second-Degree Inequalities and Nonlinear Sstems O ne

More information

Section 0.4 Inverse functions and logarithms

Section 0.4 Inverse functions and logarithms Section 0.4 Inverse functions and logarithms (5/3/07) Overview: Some applications require not onl a function that converts a numer into a numer, ut also its inverse, which converts ack into. In this section

More information

AN EFFICIENT MOVING MESH METHOD FOR A MODEL OF TURBULENT FLOW IN CIRCULAR TUBES *

AN EFFICIENT MOVING MESH METHOD FOR A MODEL OF TURBULENT FLOW IN CIRCULAR TUBES * Journal of Computational Mathematics, Vol.27, No.2-3, 29, 388 399. AN EFFICIENT MOVING MESH METHOD FOR A MODEL OF TURBULENT FLOW IN CIRCULAR TUBES * Yin Yang Hunan Ke Laborator for Computation and Simulation

More information

Review of the Fundamentals of Groundwater Flow

Review of the Fundamentals of Groundwater Flow Review of te Fundamentals of Groundwater Flow Darc s Law 1 A 1 L A or L 1 datum L : volumetric flow rate [L 3 T -1 ] 1 : draulic ead upstream [L] A : draulic ead downstream [L] : draulic conductivit [L

More information

Miniaturization of Electromagnetic Bandgap (EBG) Structures with High-permeability Magnetic Metal Sheet

Miniaturization of Electromagnetic Bandgap (EBG) Structures with High-permeability Magnetic Metal Sheet Miniaturization of Electromagnetic Bandgap (EBG) Structures with High-permeabilit Magnetic Metal Sheet Yoshitaka Toota, Kengo Iokibe, Ruji Koga Department of Communication Network Engineering, Okaama Universit,

More information

A Hybrid Numerical Method for High Contrast. Conductivity Problems. Liliana Borcea, and George C. Papanicolaou y. June 10, 1997.

A Hybrid Numerical Method for High Contrast. Conductivity Problems. Liliana Borcea, and George C. Papanicolaou y. June 10, 1997. A Hbrid Numerical Method for High Contrast Conductivit Problems Liliana Borcea, and George C. Papanicolaou June, 997 Abstract We introduce and test etensivel a numerical method for computing ecientl current

More information

What is Fuzzy Logic? Fuzzy logic is a tool for embedding human knowledge (experience, expertise, heuristics) Fuzzy Logic

What is Fuzzy Logic? Fuzzy logic is a tool for embedding human knowledge (experience, expertise, heuristics) Fuzzy Logic Fuzz Logic Andrew Kusiak 239 Seamans Center Iowa Cit, IA 52242 527 andrew-kusiak@uiowa.edu http://www.icaen.uiowa.edu/~ankusiak (Based on the material provided b Professor V. Kecman) What is Fuzz Logic?

More information

Applications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element

Applications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element Avaiable online at www.banglaol.info angladesh J. Sci. Ind. Res. (), 77-86, 008 ANGLADESH JOURNAL OF SCIENTIFIC AND INDUSTRIAL RESEARCH CSIR E-mail: bsir07gmail.com Abstract Applications of Gauss-Radau

More information

Survey of Wave Types and Characteristics

Survey of Wave Types and Characteristics Seminar: Vibrations and Structure-Borne Sound in Civil Engineering Theor and Applications Surve of Wave Tpes and Characteristics Xiuu Gao April 1 st, 2006 Abstract Mechanical waves are waves which propagate

More information

SHORT ANSWER. Write the word or phrase that best completes each statement or answers the question.

SHORT ANSWER. Write the word or phrase that best completes each statement or answers the question. Math 100 Eam 3 Review (Chapters 5-6) Name The problems included in this review involve the important concepts covered in chapters 5 and 6. You will comlete this review in two rounds: (1) In the individual

More information

1.5. Analyzing Graphs of Functions. The Graph of a Function. What you should learn. Why you should learn it. 54 Chapter 1 Functions and Their Graphs

1.5. Analyzing Graphs of Functions. The Graph of a Function. What you should learn. Why you should learn it. 54 Chapter 1 Functions and Their Graphs 0_005.qd /7/05 8: AM Page 5 5 Chapter Functions and Their Graphs.5 Analzing Graphs of Functions What ou should learn Use the Vertical Line Test for functions. Find the zeros of functions. Determine intervals

More information

The refinement of a meteorological preprocessor for the urban environment. Ari Karppinen, Sylvain M. Joffre and Jaakko Kukkonen

The refinement of a meteorological preprocessor for the urban environment. Ari Karppinen, Sylvain M. Joffre and Jaakko Kukkonen Int. J. Environment and Pollution, Vol. 14, No. 1-6, 000 1 The refinement of a meteorological preprocessor for the urban environment Ari Karppinen, Slvain M. Joffre and Jaakko Kukkonen Finnish Meteorological

More information

Chapter 8 Notes SN AA U2C8

Chapter 8 Notes SN AA U2C8 Chapter 8 Notes SN AA U2C8 Name Period Section 8-: Eploring Eponential Models Section 8-2: Properties of Eponential Functions In Chapter 7, we used properties of eponents to determine roots and some of

More information

Title. Author(s)Tamura, Shin-ichiro; Tanaka, Yukihiro; Maris, Humphr. CitationPHYSICAL REVIEW B, 60(4): Issue Date

Title. Author(s)Tamura, Shin-ichiro; Tanaka, Yukihiro; Maris, Humphr. CitationPHYSICAL REVIEW B, 60(4): Issue Date Title Phonon group velocit and thermal conduction in supe Author(s)Tamura, Shin-ichiro; Tanaka, Yukihiro; Maris, Humphr CitationPHYSICAL REVIEW B, 60(4): 2627-2630 Issue Date 1999-07-15 Doc URL http://hdl.handle.net/2115/5917

More information

A weakly dispersive edge wave model

A weakly dispersive edge wave model Coastal Engineering 38 1999 47 5 wwwelseviercomrlocatercoastaleng Technical Note A weakl dispersive edge wave model A Sheremet ), RT Guza Center for Coastal Studies, Scripps Institution of Oceanograph,

More information

Water Flow in Open Channels

Water Flow in Open Channels The Islamic Universit of Gaza Facult of Engineering Civil Engineering Department Hdraulics - ECIV 33 Chapter 6 Water Flow in Open Channels Introduction An open channel is a duct in which the liquid flows

More information

Multiple Integration

Multiple Integration Contents 7 Multiple Integration 7. Introduction to Surface Integrals 7. Multiple Integrals over Non-rectangular Regions 7. Volume Integrals 4 7.4 Changing Coordinates 66 Learning outcomes In this Workbook

More information

NEXT-GENERATION Advanced Algebra and Functions

NEXT-GENERATION Advanced Algebra and Functions NEXT-GENERATIN Advanced Algebra and Functions Sample Questions The College Board The College Board is a mission-driven not-for-profit organization that connects students to college success and opportunit.

More information

SOLVING SOME PHYSICAL PROBLEMS USING THE METHODS OF NUMERICAL MATHEMATICS WITH THE HELP OF SYSTEM MATHEMATICA

SOLVING SOME PHYSICAL PROBLEMS USING THE METHODS OF NUMERICAL MATHEMATICS WITH THE HELP OF SYSTEM MATHEMATICA SOLVING SOME PHYSICAL PROBLEMS USING THE METHODS OF NUMERICAL MATHEMATICS WITH THE HELP OF SYSTEM MATHEMATICA Pavel Trojovský Jaroslav Seibert Antonín Slabý ABSTRACT Ever future teacher of mathematics

More information

Math RE - Calculus I Exponential & Logarithmic Functions Page 1 of 9. y = f(x) = 2 x. y = f(x)

Math RE - Calculus I Exponential & Logarithmic Functions Page 1 of 9. y = f(x) = 2 x. y = f(x) Math 20-0-RE - Calculus I Eponential & Logarithmic Functions Page of 9 Eponential Function The general form of the eponential function equation is = f) = a where a is a real number called the base of the

More information

CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL

CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL Mathematical and Computational Applications,Vol. 15, No. 4, pp. 742-761, 21. c Association for Scientific Research CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL R. Naz 1,

More information

Progressive wave: a new multisource vibration technique to assist forming processes - kinematic study, simulation results and design proposition

Progressive wave: a new multisource vibration technique to assist forming processes - kinematic study, simulation results and design proposition Progressive wave: a new multisource vibration technique to assist forming processes - kinematic stud, simulation results and design proposition A. Khan a, T. H. Nguen a, C. Giraud-Audine a, G. Abba b,

More information

HSML Honors or AP Calculus Course Preparedness Test

HSML Honors or AP Calculus Course Preparedness Test HSML Honors or AP Calculus Course Preparedness Test High School Math Live wants parents to be well informed. We want our student to be placed in the appropriate course so that the will be successful and

More information

Gregory Hartman, Ph.D. Contributing Authors Troy Siemers, Ph.D. Brian Heinold, Ph.D. Dimplekumar Chalishajar, Ph.D. Editor Jennifer Bowen, Ph.D.

Gregory Hartman, Ph.D. Contributing Authors Troy Siemers, Ph.D. Brian Heinold, Ph.D. Dimplekumar Chalishajar, Ph.D. Editor Jennifer Bowen, Ph.D. AP E XCalculus I Version 30 Custom Edition for Math 00, Universit of Lethbridge Gregor Hartman, PhD Department of Applied Mathematics Virginia Militar Institute Contributing Authors Tro Siemers, PhD Department

More information

ab is shifted horizontally by h units. ab is shifted vertically by k units.

ab is shifted horizontally by h units. ab is shifted vertically by k units. Algera II Notes Unit Eight: Eponential and Logarithmic Functions Sllaus Ojective: 8. The student will graph logarithmic and eponential functions including ase e. Eponential Function: a, 0, Graph of an

More information

ONLINE PAGE PROOFS. Exponential functions Kick off with CAS 11.2 Indices as exponents

ONLINE PAGE PROOFS. Exponential functions Kick off with CAS 11.2 Indices as exponents . Kick off with CAS. Indices as eponents Eponential functions.3 Indices as logarithms.4 Graphs of eponential functions.5 Applications of eponential functions.6 Inverses of eponential functions.7 Review

More information

Linear and Nonlinear Systems of Equations. The Method of Substitution. Equation 1 Equation 2. Check (2, 1) in Equation 1 and Equation 2: 2x y 5?

Linear and Nonlinear Systems of Equations. The Method of Substitution. Equation 1 Equation 2. Check (2, 1) in Equation 1 and Equation 2: 2x y 5? 3330_070.qd 96 /5/05 Chapter 7 7. 9:39 AM Page 96 Sstems of Equations and Inequalities Linear and Nonlinear Sstems of Equations What ou should learn Use the method of substitution to solve sstems of linear

More information

Jones & Bartlett Learning, LLC NOT FOR SALE OR DISTRIBUTION. Jones & Bartlett Learning, LLC NOT FOR SALE OR DISTRIBUTION

Jones & Bartlett Learning, LLC NOT FOR SALE OR DISTRIBUTION. Jones & Bartlett Learning, LLC NOT FOR SALE OR DISTRIBUTION FIRST-ORDER DIFFERENTIAL EQUATIONS 2 Chapter Contents 2. Solution Curves without a Solution 2.. Direction Fields 2..2 Jones Autonomous & Bartlett First-Order Learning, DEs LLC 2.2 Separable Equations 2.3

More information

FRIEDRICH-ALEXANDER-UNIVERSITÄT ERLANGEN-NÜRNBERG. Lehrstuhl für Informatik 10 (Systemsimulation)

FRIEDRICH-ALEXANDER-UNIVERSITÄT ERLANGEN-NÜRNBERG. Lehrstuhl für Informatik 10 (Systemsimulation) FRIEDRICH-ALEXANDER-UNIVERSITÄT ERLANGEN-NÜRNBERG INSTITUT FÜR INFORMATIK (MATHEMATISCHE MASCHINEN UND DATENVERARBEITUNG) Lehrstuhl für Informatik 1 (Sstemsimulation) Efficient hierarchical grid coarsening

More information

BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS

BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS Koung-Heog LEE 1, Subhash C GOEL 2 And Bozidar STOJADINOVIC 3 SUMMARY Full restrained beam-to-column connections in steel moment resisting frames have been

More information

OPTIMAL CONTROL FOR A PARABOLIC SYSTEM MODELLING CHEMOTAXIS

OPTIMAL CONTROL FOR A PARABOLIC SYSTEM MODELLING CHEMOTAXIS Trends in Mathematics Information Center for Mathematical Sciences Volume 6, Number 1, June, 23, Pages 45 49 OPTIMAL CONTROL FOR A PARABOLIC SYSTEM MODELLING CHEMOTAXIS SANG UK RYU Abstract. We stud the

More information

f 0 ab a b: base f

f 0 ab a b: base f Precalculus Notes: Unit Eponential and Logarithmic Functions Sllabus Objective: 9. The student will sketch the graph of a eponential, logistic, or logarithmic function. 9. The student will evaluate eponential

More information