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Scattering_II

Course: PHYSICS 751, Fall 2007
School: UVA
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Scattering: More the Partial Wave Expansion Michael Fowler 1/17/08 Plane Waves and Partial Waves We are considering the solution to Schrdingers equation for scattering of an incoming plane wave in the z-direction by a potential localized in a region near the origin, so that the total wave function beyond the range of the potential has the form ( r , , ) = eikr cos + f ( , ) eikr . r The overall...

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Scattering: More the Partial Wave Expansion Michael Fowler 1/17/08 Plane Waves and Partial Waves We are considering the solution to Schrdingers equation for scattering of an incoming plane wave in the z-direction by a potential localized in a region near the origin, so that the total wave function beyond the range of the potential has the form ( r , , ) = eikr cos + f ( , ) eikr . r The overall normalization is of no concern, we are only interested in the fraction of the ingoing wave that is scattered. Clearly the outgoing current generated by scattering into a solid angle d at angle , is f ( , ) d multiplied by a velocity factor that also appears in the 2 incoming wave. Many potentials in nature are spherically symmetric, or nearly so, and from a theorists point of view it would be nice if the experimentalists could exploit this symmetry by arranging to send in spherical waves corresponding to different angular momenta rather than breaking the symmetry by choosing a particular direction. Unfortunately, this is difficult to arrange, and we must be satisfied with the remaining azimuthal symmetry of rotations about the ingoing beam direction. In fact, though, a full analysis of the outgoing scattered waves from an ingoing plane wave yields the same information as would spherical wave scattering. This is because a plane wave can actually be written as a sum over spherical waves: eik .r = eikr cos = i l (2l + 1) jl ( kr ) Pl (cos ) l Visualizing this plane wave flowing past the origin, it is clear that in spherical terms the plane wave contains both incoming and outgoing spherical waves. As we shall discuss in more detail in the next few pages, the real function jl (kr ) is a standing wave, made up of incoming and outgoing waves of equal amplitude. We are, obviously, interested only in the outgoing spherical waves that originate by scattering from the potential, so we must be careful not to confuse the pre-existing outgoing wave components of the plane wave with the new outgoing waves generated by the potential. The radial functions jl (kr ) appearing in the above expansion of a plane wave in its spherical components are the spherical Bessel functions, discussed below. The azimuthal rotational symmetry of plane wave + spherical potential around the direction of the ingoing wave ensures that the angular dependence of the wave function is just Pl (cos ) , not Ylm ( , ) . The coefficient 2 i l ( 2l + 1) is derived in Landau and Lifshitz, 34, by comparing the coefficient of ( kr cos ) on n the two sides of the equation: as we shall see below, ( kr ) does not appear in jl ( kr ) for l greater n than n, and ( cos ) does not appear in Pl (cos ) for l less than n, so the combination n ( kr cos ) n only occurs oncein the nth term, and the coefficients on both sides of the equation can be matched. (To get the coefficient right, we must of course specify the normalizations for the Bessel functionsee belowand the Legendre polynomial.) Mathematical Interval: The Spherical Bessel and Neumann Functions The plane wave eik .r is a trivial solution of Schrdingers equation with zero potential, and therefore, since the Pl (cos ) form a linearly independent set, each term jl (kr ) Pl ( cos ) in the plane wave series must be itself a solution to the zero-potential Schrdingers equation. It follows that jl (kr ) satisfies the zero-potential radial Schrdinger equation: l ( l + 1) d2 2d Rl ( r ) + Rl ( r ) + k 2 Rl ( r ) = 0. 2 dr r dr r2 The standard substitution Rl ( r ) = ul ( r ) / r yields d 2ul ( r ) 2 l ( l + 1) +k u (r ) = 0 dr 2 r2 For the simple case l = 0 the two solutions are u0 ( r ) = sin kr , cos kr . The corresponding radial functions R0(r) are (apart from overall constants) the zeroth-order Bessel and Neumann functions respectively. The standard normalization for the zeroth-order Bessel function is j0 ( kr ) = sin kr , kr and the zeroth-order Neumann function n0 ( kr ) = cos kr . kr Note that the Bessel function is the one well-behaved at the origin: it could be generated by integrating out from the origin with initial boundary conditions of value one, slope zero. 3 Here is a plot of j0 ( kr ) and n0 (kr ) from kr = 0.1 to 20: For nonzero l, near the origin is Rl (r ) r l or r ( ) . The well-behaved r l solution is the Bessel function, the singular function the Neumann function. The standard normalizations of these functions are given below. l +1 Here are j5 (kr ) and j50 (kr ) : 4 Detailed Derivation of Bessel and Neumann Functions This subsection is just here for completeness. We use the dimensionless variable = kr. To find the higher l solutions, we follow a clever trick given in Landau and Lifshitz (33). Factor out the l behavior near the origin by writing 5 Rl = ( ) l ( ) . l The function l ( ) satisfies 2 ( l + 1) d d2 l ( ) + ( ) + l ( ) = 0. 2 d l d The trick is to differentiate this equation with respect to : 2 ( l + 1) d 2 2 ( l + 1) d d3 l ( ) + l ( ) + 1 ( ) = 0. 3 2 d 2 d l d Writing purely formally d l ( ) = l +1 ( ) , the equation becomes d 2 (l + 2) d d2 l +1 ( ) + ( ) + l +1 ( ) = 0. 2 d l +1 d But this is the equation that l +1 ( ) must obey! So we have a recursion formula for generating all the jl ( ) from the zeroth one: l +1 ( ) = 1d l l ( ) , and jl ( ) = ( ) l ( ) , up to a d normalization constant fixed by convention. In fact, the standard normalization is l 1 d sin jl ( ) = ( ) . d l Now n ( sin ) / = ( 1) 2 n / ( 2n + 1)! 0 This is a sum of only even powers of . It is easily checked that operating on this series with l 1 d can never generate any negative powers of . It follows that jl ( ) , written as a power d series in , has leading term proportional to l. The coefficient of this leading term can be found by applying the differential operator to the series for ( sin ) / , 6 jl ( ) l ( 2l + 1)!! as 0. This r l behavior near the origin is the usual well-behaved solution to Schrdingers equation in the region where the centrifugal term dominates. Note that the small behavior is not immediately evident from the usual presentation of the jl ( ) s, written as a mix of powers and trigonometric functions, for example j1 ( ) = sin 2 cos 3 1 3cos j2 ( ) = 3 sin , etc. 2 , Turning now to the behavior of the jl ( ) s for large , from l 1 d sin jl ( ) = ( ) d l it is evident that the dominant term in the large regime (the one of order 1/) is generated by differentiating only the trigonometric function at each step. Each such differentiation can be seen to be equivalent to multiplying by (-1) and subtracting p/2 from the argument, so jl ( ) l sin as . 2 1 These jl ( ) , then, are the physical partial-wave solutions to the Schrdinger equation with zero potential. When a potential is turned on, the wave function near the origin is still l (assuming, as we always do, that the potential is negligible compared with the l ( l + 1) / 2 term sufficiently close to the origin). The wave function beyond the range of the potential can be found numerically in principle by integrating out from the origin, and in fact will be like jl ( ) above except that there will be an extra phase factor, called the phase shift and denoted by ) in the sine. The significance of this is that in the far region, the wave function is a linear combination of the Bessel function and the Neumann function (the solution to the zero-potential Schrdinger equation singular at the origin). It is therefore necessary to review the Neumann functions as well. As stated above, the l = 0 Neumann function is n0 ( ) = the minus sign being the standard convention. cos , 7 An argument parallel to the one above for the Bessel functions establishes that the higher-order Neumann functions are given by: l 1 d cos nl ( ) = ( ) . d l Near the origin nl ( ) ( 2l 1)!! as 0 l +1 and for large nl ( ) l cos as , 2 1 l sin + asymptotically can be written as a linear 2 combination of Bessel and Neumann functions in that region. so a function of the form 1 Finally, the spherical Hankel functions are just the combinations of Bessel and Neumann functions that look like outgoing or incoming plane waves in the asymptotic region: hl ( ) = jl ( ) + inl ( ) , hl * ( ) = jl ( ) inl ( ) , so for large , hl ( ) ei( l / 2) e i( l / 2) , hl * ( ) . i i The Partial Wave Scattering Matrix Let us imagine for a moment that we could just send in a (time-independent) spherical wave, with variation given by Pl(cos). For this l th partial wave (dropping overall normalization constants as usual) the radial function far from the origin for zero potential is i kr l / 2 ) + i kr l / 2 ) 1 l i e ( e( jl ( kr ) sin kr = . kr 2 2k r r If now the (spherically symmetric) potential is turned on, the only possible change to this standing wave solution in the faraway region (where the potential is zero) is a phase shift : 8 l sin kr 2 l sin kr + l ( k ) . 2 This is what we would find on integrating the Schrdinger equation out from nonsingular behavior at the origin. But in practice, the ingoing wave is given, and its phase cannot be affected by switching on the potential. Yet we must still have the solution to the same Schrdinger equation, so to match with i k the result above we multiply the whole partial wave function by the phase factor e l ( ) . The result is to put twice the phase change onto the outgoing wave, so that when the potential is switched on the change in the asymptotic wave function must be i e 2k i ( kr l / 2 ) r e + i ( kr l / 2 ) r i kr l / 2 ) S ( k ) e + i( kr l / 2) i e ( l . 2k r r This equation introduces the scattering matrix Sl ( k ) = e 2il ( k ) , which must lie on the unit circle |S| =1 to conserve probabilitythe outgoing current must equal the ingoing current. If there is no scattering, that is, zero phase shift, the scattering matrix is unity. It should be noted that when the radial Schrdingers equation is solved for a nonzero potential by integrating out from the origin, with = 0 and = 1 initially, the real function thus generated differs from the wave function given above by an overall phase factor e i l ( k ) . Scattering of a Plane Wave Were now ready to take the ingoing plane wave, break it into its partial wave components corresponding to different angular momenta, have the partial waves individually phase shifted by l-dependent phases, and add it all back together to get the original plane wave plus the scattered wave. We are only interested here in the wave function far away from the potential. In this region, the original plane wave is eik .r = eikr cos = i l (2l + 1) jl ( kr ) Pl (cos ) = i l (2l + 1) l l i e 2k i ( kr l / 2 ) Switching on the potential phase shifts factor the outgoing wave: r e + i ( kr l / 2 ) r Pl (cos ). 9 e Sl ( k ) e ( r + i kr l / 2 ) + i ( kr l / 2 ) r The actual scattering by the potential is the difference these between two terms. The complete wave function in the far region (including the incoming plane wave) is therefore: ( r , , ) = eikr cos + ( 2l + 1) l ( S ( k ) 1) P eikr l ( cos ) l 2ik r . The i l factor cancelled the e il / 2 . The -1 in ( Sl ( k ) 1) is there because zero scattering means S = 1 . Alternatively, it could be regarded as subtracting off the outgoing waves already present in the plane wave, as discussed above. There is no -dependence since with the potential being spherically-symmetric the whole problem is azimuthally-symmetric about the direction of the incoming wave. It is perhaps worth mentioning that for scattering in just one partial wave, the outgoing current is equal to the ingoing current, whether there is a phase shift or not. So, if switching on the potential does not affect the total current scattered in any partial wave, how can it cause any scattering? The point is that for an ingoing plane wave with zero potential, the ingoing and outgoing components have the right relative phase to add to a component of a plane wavea tautology, perhaps. But if an extra phase is introduced into the outgoing wave only, the ingoing + outgoing will no longer give a plane wavethere will be an extra outgoing part proportional to ( Sl ( k ) 1) . Recall that the scattering amplitude f ( , ) was defined in terms of the solution to Schrdingers equation having an ingoing plane wave by ( r , , ) = e ikr cos eikr + f ( , ) . r Were now ready to express the scattering amplitude in terms of the partial wave phase shifts (for a spherically symmetric potential, of course): f ( , ) = f ( ) = ( 2l + 1) l ( S ( k ) 1) P l 2ik l ( cos ) = ( 2l + 1) fl ( k ) Pl ( cos ) l where fl ( k ) = 1 i l ( k ) sin l ( k ) e k is called the partial wave scattering amplitude, or just the partial wave amplitude. 10 So the total scattering amplitude is the sum of these partial wave amplitudes: f ( ) = 1 ( 2l + 1) eil ( k ) sin l ( k ) Pl ( cos ). kl The total scattering cross-section = f ( ) 2 d = 2 f ( ) 2 sin d 0 = 2 0 2 1 ( 2l + 1) eil ( k ) sin l ( k ) Pl ( cos ) sin d kl and the normalization of the Legendre polynomials 2 P ( cos ) sin d = 2l + 1 2 l 0 gives = 4 ( 2l + 1) f l ( k ) = l =0 2 4 k2 ( 2l + 1) sin l =0 2 l . So the total cross-section is the sum of the cross-sections for each l value. This does not mean, though, that the differential cross-section for scattering into a given solid angle is a sum over separate l valuesthe different components interfere. It is only when all angles are integrated over that the orthogonality of the Legendre polynomials guarantees that the cross-terms vanish. Notice that the maximum possible scattering cross-section for particles in angular momentum state l is ( 4 / k 2 ) ( 2l + 1) , which is four times the classical cross section for that partial wave impinging on, say, a hard sphere! (Imagine semiclassically particles in an annular area: angular momentum L = rp, say, but L = l and p = k so l = rk. Therefore the annular area corresponding to angular momentum between l and l + 1 has inner and outer radii l / k and ( l + 1) / k and therefore area ( 2l + 1) / k 2 .) The quantum result is essentially a diffractive effect, well discuss it more later. Its easy to prove the optical theorem for a spherically-symmetric potential: just take the imaginary part of each side of the equation f ( ) = 1 ( 2l + 1) eil ( k ) sin l ( k ) Pl ( cos ) kl 11 at = 0, using Pl (1) = 1, Im f ( = 0 ) = 1 ( 2l + 1) sin 2 l ( k ) kl from which the optical theorem Im f ( 0 ) = k / 4 follows immediately. Its also worth noting what the unitarity of the lth partial wave scattering matrix Sl Sl = 1 implies 1 for the partial wave amplitude fl ( k ) = ei l ( k ) sin l ( k ) . Since Sl ( k ) = e 2il ( k ) , it follows that k Sl ( k ) = 1 + 2ikfl ( k ) . From this, Sl Sl = 1 gives: Im f l ( k ) = k fl ( k ) . 2 This can be put more simply: Im 1 = k . fl ( k ) In fact, fl ( k ) = 1 k ( cot l ( k ) i ) . Phase Shifts and Potentials: Some Examples We assume in this section that the potential can be taken to be zero beyond some boundary radius b. This is an adequate approximation for all potentials found in practice except the Coulomb potential, which will be discussed separately later. Asymptotically, then, i e i( kr l / 2) e 2il ( k ) e + i( kr l / 2) l (r ) = 2k r r = = eil ( k ) sin ( kr + l ( k ) l / 2 ) kr e i l ( k ) kr ( sin ( kr l / 2 ) cos ( k ) + cos ( kr l / 2 ) sin ( k ) ) . l l 12 This expression is only exact in the limit r , but since the potential can be taken zero beyond r = b, the wave function must have the form l ( r ) = ei ( k ) ( cos l ( k ) jl ( kr ) sin l ( k ) nl ( kr ) ) l for r > b. (The - sign comes from the standard convention for Bessel and Neumann functionssee earlier.) The Hard Sphere The simplest example of a scattering potential: V ( r ) = for r < R, V ( r ) = 0 for r R. The wave function must equal zero at r = R, so from the above form of l ( r ) , tan l ( k ) = For l = 0, tan 0 ( k ) = jl ( kR ) . nl ( kR ) ( sin kR ) / kR = tan kR, ( cos kR ) / kR so 0 ( k ) = kR. This amounts to the wave function being effectively moved over to begin at R instead of at the origin: sin k ( r + ) sin k ( r R ) sin kr = kr kr kr for r > R, of course = 0 for r < R. For higher angular momentum states at low energies (kR << 1), j ( kR ) ( kR ) / ( 2l + 1)!! = ( kR ) tan l ( k ) = l . l +1 2 nl ( kR ) ( 2l 1)!!/ ( kR ) ( 2l + 1) ( ( 2l 1)!!) l 2 l +1 Therefore at low enough energy, only l = 0 scattering is importantas is obvious, since an incoming particle with momentum p = k and angular momentum l is most likely at a distance l/k from the center of the potential at closest approach, so if this is much greater than R, the phase shift will be small. 13 The Born Approximation for Partial Waves From the definition of f ( , ) k (r ) = ei k r + f ( , ) ei k r r and k ( r ) = e i k r m ei kr i k f r 3 2 d r e V (r ) k (r ) 2 r recall the Born approximation amounts to replacing the wave function k (r ) in the integral on the right by the incoming plane wave, therefore ignoring rescattering. To translate this into a partial wave approximation, we first take the incoming k to be in the zdirection, so in the integrand we replace k (r ) by eikr cos = i l (2l + 1) jl (kr ) Pl (cos ). l Labeling the angle between k f and r by , e i k f r = ( i ) (2l + 1) jl (kr ) Pl (cos ). l l Now k f is in the direction ( , ) and r in the direction ( , ) , and is the angle between them. For this situation, there is an addition theorem for spherical harmonics: Pl ( cos ) = 4 l * Ylm ( , ) Ylm ( , ) . 2l + 1 m = l On inserting this expression and integrating over , , the nonzero m terms give zero, in fact the only nonzero term is that with the same l as the term in the k (r ) expansion, giving f ( ) = 2m 2 ( 2l + 1)P ( cos ) r drV ( r ) ( j ( kr ) ) 2 l =0 l 2 l 0 and remembering f ( ) = 1 ( 2l + 1) eil ( k ) sin l ( k ) Pl ( cos ) kl it follows that for small phase shifts (the only place its valid) the partial-wave Born approximation reads 14 l ( k ) 2mk r drV ( r ) ( j ( kr ) ) 2 l 2 2 . 0 Low Energy Scattering: the Scattering Length From fl ( k ) = k ( cot l ( k ) i ) the l = 0 cross section is l =0 = 1 4 k 2 cot 0 ( k ) i 2 , . At energy E 0, the radial Schrdinger equation for u = r away from the potential becomes d 2u / dr 2 = 0 , with a straight line solution u ( r ) = C ( r a ) . This must be the k 0 limit of u ( r ) = C sin ( kr + 0 ( k ) ) , which can only be correct if 0 is itself linear in k for sufficiently small k, and then it must be 0 ( k ) = ka, a being the point at which the extrapolated external wavefunction intersects the axis (maybe at negative r!) So, as k goes to zero, the cot term dominates in the denominator and l =0 ( k 0 ) = 4 a 2 . The quantity a is called the scattering length. Integrating the zero-energy radial Schrdinger equation out from u(r) = 0 at the origin for a weak (spherical) square well potential, it is easy to check that a is positive for a repulsive potential, negative for an attractive potential. Repulsive potential, zero-energy wave function (so its a straight line outside of the well!): 15 Scattering Length for Square W ell 2 1 0 -5 0 5 10 -1 -2 Potential Tangent Wavef unction Attractive potential: S cattering Length for Square W ell 2 1 0 -5 0 5 10 -1 -2 Potential Tangent Wavef unction On increasing the strength of the repulsive potential, still solving for the zero-energy wave function, a tends to the potential wallheres the zero-energy wavefunction for a barrier of height 6: 16 Scattering Length for Square W ell 1 0 -5 0 5 10 -1 Potential Tangent Wavef unction For an infinitely high barrier, the wave function is pushed out of the barrier completely, and the hard sphere result is recovered: scattering length a, cross-section 4 a2. On increasing the strength of the attractive well, if there is a phase change greater that /2 within the well, a will become positive. In fact, right at /2, a is infinite! S cattering Length for Square W ell 2 1 0 -5 0 5 -1 -2 Potential Tangent Wavef unction And a little more depth to the well gives a positive scattering length: 10 17 Scattering Length for Square W ell 2 1 0 -5 0 5 10 -1 -2 Potential Tangent Wavef unction In fact, a well deep enough to have a positive scattering length will also have a bound state. This becomes evident when one considers that the depth at which the scattering length becomes infinite can be thought of as formally having a zero energy bound state, in that although the wave function outside is not normalizable, it is equivalent to an exponentially decaying function with infinite decay length. If one now deepens the well a little, the zero-energy wave function inside the well curves a little more rapidly, so the slope of the wave function at the edge of the well becomes negative, as in the picture above. With this slightly deeper well, we can now lower the energy slightly to negative values. This will have little effect on the wave function inside the well, but make possible a fit at the well edge to an exponential decay outsidea genuine bound state, with wave function e r outside the well. 0.5 0 0 5 10 15 - 0.5 Potential Wavef unction 20 25 30 18 If the binding energy of the state is really low, the zero-energy scattering wave function inside the well is almost identical to that of this very low energy bound state, and in particular the logarithmic derivative at the wall will be very close, so 1 / a , taking a to be much larger than the radius of the well. This connects the large scattering length to the energy of the weakly bound state, B. E. = 2 k 2 / 2m = 2 / 2ma 2 . (Sakurai, p 414.) Wigner was the first to use this to estimate the binding energy of the deuteron from the observed cross section for low energy neutron-proton scattering.
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UVA - PHYSICS - 1425
More StaticsPhysics 1425 Lecture 24Michael Fowler, UVaStatics: Conditions for Equilibrium For any body, MdvCM / dt = Fi , the net forcecauses the CM to accelerate. Hence, if the body isremaining at rest,F = 0ii To eliminate angular acceleration,
UVA - PHYSICS - 1425
HydrostaticsPhysics 1425 Lecture 25Michael Fowler, UVaBasic Concepts Density Pressure: Pascals PrincipleThe Crown and the Bathtub Around 250 BC, the king ofSyracuse commissioned a newcrown,and gave the goldsmithabout 1 kg of gold (size of a Dba
UVA - PHYSICS - 1425
More HydrostaticsPhysics 1425 Lecture 26Michael Fowler, UVaBasic Concepts Atmospheric Pressure Buoyancy: Archimedes PrincipleClicker Question Galileo once observed that even a carefullyconstructed pump, situated at ground level,was not able to dr
UVA - PHYSICS - 1425
HydrodynamicsPhysics 1425 Lecture 27Michael Fowler, UVaBasic Concepts Fluid conservation Bernoullis EquationYou are sitting in a rowing boat in a small pond. There are somebricks in the boat. You take the bricks and throw them into thepond. They s
UVA - PHYSICS - 1425
Simple Harmonic MotionPhysics 1425 Lecture 28Michael Fowler, UVaForce of a Stretched Spring If a spring is pulled toextend beyond itsnatural length by adistance x, it will pullback with a forceF = kxwhere k is called thespring constant.The sam
UVA - PHYSICS - 1425
Damped and Driven Harmonic MotionPhysics 1425 Lecture 29Michael Fowler, UVaDamped Harmonic Motion In the real world, oscillators CSprings force Drag forceexperience damping forces:F = kx F = bvfriction, air resistance, etc.m These forces always
UVA - PHYSICS - 1425
Temperature, Expansion, Ideal Gas LawPhysics 1425 Lecture 30Michael Fowler, UVaEverythings Made of Atoms This idea was only fully accepted about 100years agoin part because of Einsteinsanalysis of Brownian motion. Brown, who studied the sex life of
UVA - PHYSICS - 1425
Kinetic Theory of GasesPhysics 1425 Lecture 31Michael Fowler, UVaBernoullis Picture Daniel Bernoulli, in 1738, wasthe first to understand airpressure in terms of moleculeshe visualized them shootingaround very rapidly in a closedcontainer, suppor
UVA - PHYSICS - 1425
More Kinetic Theory of GasesPhysics 1425 Lecture 32Michael Fowler, UVaVapor Pressure and Humidity The H2O molecules in liquid water stronglyattract each other, holding the liquid together.But these molecules are still jiggling around,with a Maxwell
UVA - PHYSICS - 1425
Heat and Energy ConservationPhysics 1425 Lecture 33Michael Fowler, UVaHeat Flow If something warm is in contact with somethingqcooler, the warm thing cools down as the cool thinggets a little warmer. This flow of energy, called heat,was until the
UVA - PHYSICS - 1425
Gas Processes and Heat TransportPhysics 1425 Lecture 34Michael Fowler, UVaThe First Law of Thermodynamics A closed system has a total internal energy Eint. This energy can be changed in two different ways:A. The system can do work W, or have work do
UVA - PHYSICS - 1425
The Second Law of Thermodynamics:Heat EnginesPhysics 1425 Lecture 35Michael Fowler, UVaThe First Law of Thermodynamics In any process, total energy is always conserved. Once it was fully realized that heat is just anotherform of energy, it was esta
UVA - PHYSICS - 1425
EntropyPhysics 1425 Lecture 36Michael Fowler, UVaFirst and Second Laws ofThermodynamics A quick review. First Law: total energy conserved in anyprocess: joules in = joules out Second Law: heat only flows one way, and wecant turn heat into just wo
Auburn - PHYS - 2200
Physics 1425: General Physics ISpring 2010Michael FowlerRoom 307, PhysicsHome PageTodays Topics Course arrangements, syllabus outline. Nature of science: observation andmeasurement. Accuracy, significant figures. Units, mass of water, estimation
Auburn - PHYS - 2200
A proposed Magnetized Dusty Plasma User FacilityE. Thomas, Jr. (Auburn Univ.), R. L. Merlino (Univ. Iowa), M. Rosenberg (UCSD)Previous experiments on magnetized dusty plasmasFeasibility of a magnetized dusty plasma facilityMPE superconducting magnet s
Auburn - PHYS - 2200
SOLUTIONSPHYS 2200 Introduction to Quantum Mechanics and RelativityEXAM 1Fall Semester, 2011Instructions:a) This exam is closed book and closed notes.b) You MUST show all of your work in order to obtain full credit on the problems.Part 1: Short Pro
Auburn - PHYS - 2200
Solutions to HW 1: Ch. 1 - 3, 4, 7, 8, 9, 20, 22, 25, 41 The problem uses the Lorentz transform approach. More explicitly, they have done the following: Earth frame: Plane frame: Dlyra = +2500 cy = x1
Auburn - PHYS - 2200
oo234x(m)(b) When 10 seconds have passed on the rocket's clock, only 6 seconds have passed onthe laboratory clock.Solutions to HW 1: Ch. 1 18, 23, 27, 43; Ch. 2 1, 4, 5, 81-18.(a)U'=0U~=0xyx'vx=UxU'x+v1 + vU.:O+V=-=VIc1+ 02
Auburn - PHYS - 2200
Solutions to HW 3: Ch. 2 12, 14, 17, 19, 24, 27, 40 -9Note: Error in text solution: 0.34 ng and 0.68 ng (n = nano = 10 ) NOT !
Ole Miss - SPAN - 102
Expresiones para la claseExpressions for the classLearn the following commands, so that you can react to them when they are used by your instructor:Comments and questions from the studentsCmo se dice en espaol?Cmo se escribe?Qu quiere decir?No enti
Ole Miss - SPAN - 102
Spanish 102 Exam 1 Study Guide - Captulo 5 - (35 points)* Please bring a purple scantron and # 2 pencils.*Receiving or giving aid on a test or an exam is cause for dismissal from the University ofMississippi. Any questions should be directed to your In
Ole Miss - SPAN - 102
STUDY GUIDE - ESPAOL 102 - EXAMEN 2 - Captulo 6 (33 points)* Please bring a purple scantron and # 2 pencils.*ACTIVIDAD A. LOS ALIMENTOS.Las descripciones de alimentos. John est en un restaurante mexicano pero no comprende elmen. Su amigo Miguel le des
Ole Miss - SPAN - 102
ESPAOL 102 - EXAMEN 3 - Captulo 7 - STUDY GUIDE* Please bring a purple scantron and # 2 pencils.*ACTIVIDAD A. Qu tiempo hace? Juana tiene que hacer un informe meteorolgico.Escucha lo que dice y selecciona la opcin correcta. (4 puntos)Modelo:You hear:
Ole Miss - SPAN - 102
ESPAOL 102 EXAMEN 4 Captulo 8 (27 puntos)* Please bring number a purple scantron sheet and number 2 pencils.*Receiving or giving aid on a test or an exam is cause for dismissal from the University ofMississippi. Any questions should be directed to your
Ole Miss - SPAN - 102
ESPAOL 102 STUDY GUIDE - EXAMEN FINAL (100 puntos)* Please do not forget your PURPLE scantron sheet and no. 2 pencils *Receiving or giving aid on a test or an exam is cause for dismissal from the University. Anyquestions should be directed to your inst
Ole Miss - SPAN - 101
Expresiones para la claseExpressions for the classLearn the following commands, so that you can react to them when they are used by your instructor:Comments and questions from the studentsCmo se dice en espaol?Cmo se escribe?Qu quiere decir?No enti
Ole Miss - SPAN - 101
SPANISH 101 STUDY GUIDE TEST 1 Captulo 1 (36 points)Please, bring a Purple Scantron No. 16485 and # 2 pencils.Receiving or giving aid on a test or an exam is cause for dismissal from the University ofMississippi. Any questions should be directed to you
Ole Miss - SPAN - 101
SPANISH 101 - STUDY GUIDE- EXAM 2 - Captulo 2 - (38 points)Please, bring a Purple Scantron No. 16485 and # 2 pencils.Receiving or giving aid on a test or an exam is cause for dismissal from the University ofMississippi. Any questions should be directed
Ole Miss - SPAN - 101
STUDY GUIDE- SPANISH 101 EXAMEN 3 - CHAPTER 3 (37 points)Please, bring a Purple Scantron No. 16485 and # 2 pencils.Receiving or giving aid on a test or an exam is cause for dismissal from the University. Anyquestions should be directed to your instruct
Ole Miss - SPAN - 101
Spanish 101 Study Guide - Exam 4 Chapter 4 (34 points)Please, bring a Purple Scantron No. 16485 and # 2 pencils.Receiving or giving aid on a test or an exam is cause for dismissal from the University of Mississippi. Anyquestions should be directed to y
Ole Miss - SPAN - 101
SPANISH 101- FINAL EXAM STUDY GUIDE - (100 points) - Fall 2011*Don't forget your purple scantron and # 2 pencil for the exam*ACTIVIDAD A. Arriba! Readings. (10 points)Choose the correct answer for each of the following questions related to the selected