The Grüneisen parameter for aluminum in the temperature range K

Similar documents
a) Use the following equation from the lecture notes: = ( J K 1 mol 1) ( ) 10 L

Statistical Mechanics, Kinetic Theory Ideal Gas. 8.01t Nov 22, 2004

Testing thermo-acoustic sound generation in water with proton and laser beams

A. Ricci, E. Giuri. Materials and Microsystems Laboratory

Energy Transport. Focus on heat transfer. Heat Transfer Mechanisms: Conduction Radiation Convection (mass movement of fluids)

CLASSICAL CONCEPT REVIEW 8

Solid State Detectors = Semi-Conductor based Detectors

No Evidence for a new phase of dense hydrogen above 325 GPa

Chapter Test B. Chapter: Measurements and Calculations

IDEAL AND NON-IDEAL GASES

A Theory for the Cosmological Constant and its Explanation of the Gravitational Constant

Problem Set 3 Solutions

Plate waves in phononic crystals slabs

7. DYNAMIC LIGHT SCATTERING 7.1 First order temporal autocorrelation function.

Physics 9e/Cutnell. correlated to the. College Board AP Physics 1 Course Objectives

State Newton's second law of motion for a particle, defining carefully each term used.

Answer, Key Homework 6 David McIntyre 1

Physics Notes Class 11 CHAPTER 2 UNITS AND MEASUREMENTS

TEMPERATURE DEPENDENCE OF GRAVITATIONAL FORCE: EXPERIMENTS, ASTROPHYSICS, PERSPECTIVES. A.L. Dmitriev

Steady Heat Conduction

Thermodynamics: Lecture 2

BIOMEDICAL ULTRASOUND

Differential Relations for Fluid Flow. Acceleration field of a fluid. The differential equation of mass conservation

Pressure in Fluids. Introduction

Indiana's Academic Standards 2010 ICP Indiana's Academic Standards 2016 ICP. map) that describe the relationship acceleration, velocity and distance.

PHY1020 BASIC CONCEPTS IN PHYSICS I

Gravimetric determination of pipette errors

arxiv:astro-ph/ v1 15 Sep 2005

AP Physics 1 and 2 Lab Investigations

Chapter 18 Temperature, Heat, and the First Law of Thermodynamics. Problems: 8, 11, 13, 17, 21, 27, 29, 37, 39, 41, 47, 51, 57

Dynamic Process Modeling. Process Dynamics and Control

State Newton's second law of motion for a particle, defining carefully each term used.

The first law: transformation of energy into heat and work. Chemical reactions can be used to provide heat and for doing work.

Preview of Period 2: Forms of Energy

ENERGY CONSERVATION The First Law of Thermodynamics and the Work/Kinetic-Energy Theorem

When the fluid velocity is zero, called the hydrostatic condition, the pressure variation is due only to the weight of the fluid.

Carbon Cable. Sergio Rubio Carles Paul Albert Monte

Experiment 12E LIQUID-VAPOR EQUILIBRIUM OF WATER 1

Carbon Dioxide and an Argon + Nitrogen Mixture. Measurement of C p /C v for Argon, Nitrogen, Stephen Lucas 05/11/10

Chemistry 212 VAPOR PRESSURE OF WATER LEARNING OBJECTIVES

Applying the Wheatstone Bridge Circuit

THE KINETIC THEORY OF GASES

An optical readout configuration for advanced massive GW detectors

CH3 Stoichiometry. The violent chemical reaction of bromine and phosphorus. P.76

Chem 115 POGIL Worksheet - Week 4 Moles & Stoichiometry

Fall 2004 Ali Shakouri

Gas Chromatography. Let s begin with an example problem: SPME head space analysis of pesticides in tea and follow-up analysis by high speed GC.

Stability of Evaporating Polymer Films. For: Dr. Roger Bonnecaze Surface Phenomena (ChE 385M)

Modification of Pd-H 2 and Pd-D 2 thin films processed by He-Ne laser

OPTIMAL DESIGN AND OPERATION OF HELIUM REFRIGERATION SYSTEMS *

World of Particles Big Bang Thomas Gajdosik. Big Bang (model)

CFD Application on Food Industry; Energy Saving on the Bread Oven

8.2 Elastic Strain Energy

99.37, 99.38, 99.38, 99.39, 99.39, 99.39, 99.39, 99.40, 99.41, cm

Millikan Oil Drop Experiment Matthew Norton, Jurasits Christopher, Heyduck William, Nick Chumbley. Norton 0

Thermodynamics AP Physics B. Multiple Choice Questions

J.Instrum.Soc.India 30(1)29-34 PROGRAMMABLE CONTROL OF TEMPERATURE: A SIMPLE AND VERSATILE METHOD. N. Asha Bhat and K. S. Sangunni.

k L a measurement in bioreactors

Chapter 1: Chemistry: Measurements and Methods

Politecnico di Torino. Porto Institutional Repository

Free Electron Fermi Gas (Kittel Ch. 6)

KINETIC THEORY AND THERMODYNAMICS

THE IDEAL GAS LAW AND KINETIC THEORY

Refractive Index Measurement Principle

Temperature. Temperature

The Viscosity of Fluids

Integration of a fin experiment into the undergraduate heat transfer laboratory

4 Thermomechanical Analysis (TMA)

Vacuum Evaporation Recap

Laser-induced surface phonons and their excitation of nanostructures

The Second Law of Thermodynamics

Conservation of Momentum and Energy

Chapter Outline. Diffusion - how do atoms move through solids?

Experimental and Predicted Performance of the BEI Mini-Linear Cooler

MIME 3330 Mechanics Laboratory LAB 5: ROTATING BENDING FATIGUE

Statistical Rules of Thumb

A HIGH GAIN OPERATING REGIME FOR THE FREQUENCY TO VOLTAGE CONVERTER *

Waves: Recording Sound Waves and Sound Wave Interference (Teacher s Guide)

Appendix I: Cryogenic Reference Tables

Physical Chemistry Laboratory I CHEM 445 Experiment 6 Vapor Pressure of a Pure Liquid (Revised, 01/09/06)

) and mass of each particle is m. We make an extremely small

Thermal Resistance, Power Dissipation and Current Rating for Ceramic and Porcelain Multilayer Capacitors

Calculating particle properties of a wave

Thermochemistry. r2 d:\files\courses\ \99heat&thermorans.doc. Ron Robertson

Experiment #4, Ohmic Heat

Application of the Orifice Meter for Accurate Gas Flow Measurement page 1. Application of the Orifice Meter for Accurate Gas Flow Measurement.

A Performance Comparison of Vapour Compression Refrigeration System Using Eco Friendly Refrigerants of Low Global Warming Potential

Mesh Discretization Error and Criteria for Accuracy of Finite Element Solutions

Unit 3: States of Matter Practice Exam

Physics Lab Report Guidelines

1 The basic equations of fluid dynamics

Topic 3b: Kinetic Theory

CHEMISTRY. Matter and Change. Section 13.1 Section 13.2 Section The Gas Laws The Ideal Gas Law Gas Stoichiometry

Thermodynamics. Chapter 13 Phase Diagrams. NC State University

Notes on Elastic and Inelastic Collisions

Bruce B. Weiner, Walther W. Tscharnuter, David Fairhurst Brookhaven Instruments Corporation Holtsville, NY US

Lab 9: The Acousto-Optic Effect

TIE-31: Mechanical and thermal properties of optical glass

E X P E R I M E N T 8

CHAPTER 12. Gases and the Kinetic-Molecular Theory

Transcription:

The Grüneisen parameter for aluminum in the temperature range 0.3-1.1 K Alessandro Marini INFN-Laboratori Nazionali di Frascati, Via E. Fermi 40, I-00044 Frascati, Italy Available critical field data as a function of temperature and pressure are used to calculate the electronic contribution to the Grüneisen parameter for pure aluminum in the superconducting state. Large negative values for the parameter are found in the range of temperatures of interest starting from the value γ e s(t = T c )= 10.7 ± 0.8. This fact could be taken into account as a possible explanation for the cosmic ray large signals detected at a rate higher than expected by the gravitational wave antenna NAUTILUS when operated in superconducting regime. PACS numbers: 74.5.-q, 65.40.-b. 1. INTRODUCTION Studies 1 3 of the signals due to the interactions of cosmic rays impinging on the gravitational wave antenna NAUTILUS, a massive (.3 ton) bar made of an aluminum alloy, have shown that in a run of the detector at thermodynamic temperature T = 1.5K the results are in agreement with the thermo-acoustic model, while in a run at T = 0.14K large signals are detected at a rate higher than expected. In the thermo-acoustic model mechanical vibrations originate from the local thermal expansion caused by warming up due to the energy lost by a particle crossing the material. More precisely, the relation that accounts for the detectable vibrational energy E in the n th longitudinal mode due to a specific energy loss dw/dx of a particle impinging on a cylindrical bar is: 4 E = 4k γ 9π ρlv (dw dx ) F n (z 0,θ 0,l 0 ) where k is the Boltzmann constant, ρ is the density of the bar material,

A.Marini L is the length of the bar, v is the longitudinal speed of sound, γ is the Grüneisen adimensional parameter of the material and F n is a function of the impinging track geometrical parameters, not relevant in this context. The thermo-acoustic model predictions have been recently verified by an experiment, 5 operated only at room temperature, using a small suspended aluminum cylinder exposed to an electron beam. The experiment was also motivated by the applicability of the model in the evaluation of the cosmic ray effects on resonant mass gravitational wave detectors of ultrahigh sensitivity. The NAUTILUS results suggest that a more efficient mechanism for particle energy loss conversion into mechanical energy takes place when the bar is in the superconducting state. The behaviour of the Grüneisen parameter at ultra low temperatures is one of the various possible explanations for the observed effects in NAUTILUS. After a short review of the Grüneisen parameter properties at low temperatures and a summary of experimental results obtained for almost pure aluminum (Section ), a calculation of the electronic Grüneisen parameter based on available experimental data in the temperature range 0.3 1.1K is here reported (Section 3).. PROPERTIES OF THE GRÜNEISEN PARAMETER AT LOW TEMPERATURE AND AVAILABLE EXPERIMENTAL DATA.1. Properties of the Grüneisen parameter at low temperature The Grüneisen parameter γ is defined as: γ(t,v )= βv χ T C V where β[= ( ln V/ T) p ]isthe volume expansion coefficient, V is the molar volume, χ T [= ( ln V/ p) T ]isthe compressibility at constant temperature and C V is the specific heat at constant volume. For aluminum the thermal expansion at the critical temperature and below is too small to be measured directly by present techniques. For the normal state an extrapolation from higher temperatures is possible, but for the superconducting state a thermodinamic derivation from the experimental pressure and temperature dependence of the critical field H c can be used. Differences between normal (n) and superconducting (s) states are expected in the quantities defining the electronic component of the Grüneisen parameter. According to Shoenberg, 6 the differences are expressed in terms

Grüneisen parameter for Al below T =1.1K of the pressure and temperature dependence of the critical field. In particular, for Type I superconductors the differences in the volume expansion coefficient and compressibility are to the first order: and β n β s = 1 H c H c 4π T p + H c H c 4π p T (1) χ s χ n = 1 4π ( H c p ) + H c H c 4π p () respectively. From the definition of γ it follows that the electronic component of the Grüneisen parameter in the superconducting state is: 7 γs e = C e,n γn e V (β n β s ) C e,s χc e,s where C e,n,c e,s are the electronic contributions to the specific heat in the normal and superconducting states, γn e is the electronic component of the Grüneisen parameter in the normal state and χ s χ n is assumed (see discussion below). Using an alternate formulation of (1), that exploits the dependence of β n β s on Hc and includes the contribution of the magnetostriction in the superconducting state, the electronic Grüneisen parameter in the superconducting state can be finally expressed as: 7 γs e = C e,n γn e V 1 C e,s χc e,s 8π ( Hc T p χ H c T ) (3) At T = T c γs e takes the form: 7 γs(t e = T c )= C e,n γn e + C n C s d lnt c C e,s C e,s d lnv (4) where C n C s is the difference of the specific heats at the transition... Experimental values of the Grüneisen parameter for aluminum at low temperature Several authors have in the past measured the electronic and lattice components of the Grüneisen parameter for aluminum down to low temperatures. 8 Results have been obtained using methods based on dilatometry with capacitive readout, 9, 10 on pulsed thermoelastic stresses, 11 and on measurements of the variations of the critical field as a function of the pressure and the temperature. 1 15 The accurate results from the dilatometry, obtained at very low values of temperature but higher than the critical value (T c 1.1K), are in extremely

A.Marini good agreement with the theoretical expectations for γ 0 [.5] 8 and γ e [1.63], 16 respectively the lattice and the electronic components extrapolated at T =0. Some results for γ e, obtained from the studies of H c and characterized at T = T c, apparently deviate from those coming from dilatometry by a factor of the order approximately greater than three. This discrepancy could be due to the complexity of the experimental technique of the variations of H c with p and T,ortothe theoretical hypothesis assumed for deriving the result. 3. CALCULATION OF γ e s IN THE TEMPERATURE INTERVAL 0.3K T 1.1K The previously cited article by Harris and Mapother contains a tabulation of critical field data in the temperature range starting from T 0.3K up to T c for four values of pressure (p 0, 11, 367, 490 atm). This tabulation can be used as an input to relation (3) for calculating γs e at p =0ina temperature interval from 0.3K up to 1.1K, below T c. Relation (3) can be written in the form γs e = A B C, with A = Ce,n C e,s γn, e B = V 1 χc e,s 8π and C = Hc T p χ H c T, for evaluating the relative weight of the terms. In order to calculate A and B, the fitting functions: 1.34 Tc/T C e,n =ΓT,C e,s =7.1ΓT c e where R is the gas constant, θ = 47.7K, Γ=1.35 10 3 J/(moleK ), T c = 1.163K, are taken from Phillips 17 and γn e =1.63 is assumed. The values of A and B for some points of the temperature interval are shown in the table. The H c tabulated data are used for computing the terms Hc T p and H c T in C. The fit of Hc with a polynomial of the fourth order in T at fixed p gives directly H c T. Linear fits vs. p of H c T at fixed T give the values of Hc T p. In this approximation the second derivatives of Hc are independent of the pressure. The first term of C is greater by nearly an order of magnitude than the second, computed at p =0,but the errors on the first term, estimated from the covariance matrices and the χ of the fits, reach the maximum value of 80%. The table shows the obtained values for C for some points of the temperature interval. Relation (3) is valid in the approximation that χ s χ n, and the H c tabulated data can be used for calculating () to verify this assumption. A fitting procedure, similar to the one described above and disregarding the contribution of the second derivatives, is used to calculate Hc p at fixed T. Values of χs χn χ n are obtained ranging from 4.5 10 7 to 9.5 10 7 in the

Grüneisen parameter for Al below T =1.1K T[K] A B[10 7 K] C[10 7 K 1 ] 0.3 10.68 48.0 3.77 0.5.3 6.01.91 0.7 1.8.47 5.15 0.9 1.00 1.50 8.6 1.1 0.90 1.10 11.43 temperature interval, with an error of the order of 10% evaluated from the covariance matrices and the χ of the fits. Whit this result it is possible to use the value 18 χ =1.33 10 1 cm /dine both for the normal and the superconducting states. The final calculation of A B C gives negative values for γs, e due in this context to the prevalence respect to A of B C, whose positive sign is determined by the sign of C. However it must be underlined that C is affected by large errors, mainly due to the inaccuracy of Hc T p. Fig. 1 shows the absolute vales of γs e at p =0in the interval 0.3K T 1.1K. Agreement is found for γs(t e =1.1K) computed from the fitting procedure and γs e at T = T c computed from equation (4) using the specific heat data given by Phillips and dlntc dlnv given by Harris and Mapother: γ e s(t = T c )= 10.7 ± 0.8 4. CONCLUSIONS In this macroscopic framework, involving thermoelastic properties of pure aluminum in normal and superconducting states, the electronic Grüneisen parameter for the superconductive state, γs, e seems to have absolute values greater than those assumed in the normal state. This circumstance, possibly due to the fitting procedures and approximations used in the treatment of the available data or to the experimental accuracies, could be related to the discrepancy in the rate of high energy cosmic rays observed in NAUTILUS when operated in superconducting state. However this simplified explanation does not take into account other factors, such as the fact that the bar is not made of pure aluminum, but together with other possible explanations it could be object of investigation by means of a suspended small cylindrical bar made of the same aluminum alloy as NAUTILUS, impinged by a high energy electron beam and operated either in the normal or in the superconducting states.

A.Marini Fig. 1. Absolute values of γ e s at p =0;broken lines show the estimated errors from the covariance matrices and χ of the fits.

Grüneisen parameter for Al below T =1.1K REFERENCES 1. P. Astone et al., Phys. Rev. Lett. 84, 14(000). P. Astone et al., Phys. Lett. B 499, 16(001) 3. P. Astone et al., Phys. Lett. B 540, 179 (00) 4. See for instance: G. Liu and B. Barish, Phys. Rev. Lett. 61, 71 (1988) and references therein 5. G.D. van Albada et al., Rev. Sci. Instrum. 71, 1345 (000) 6. D. Shoenberg, Superconductivity, Cambridge Univ. Press (1965) pagg. 58,74-75 7. R.W. Munn, Phys. Rev. 178, 677 (1969) 8. A comprehensive survey on this argument can be found in: T.H.K. Barron, J.G. Collins and G.K. White, Adv. in Phys. 9, 609 (1980) 9. J.G. Collins, G.K. White and C.A. Swenson, Journ. Low Temp. Phys. 10, 69 (1973) 10. F.R. Kroeger and C.A. Swenson, Journ. Appl. Phys. 48, 853 (1977) 11. W.B. Gauster, Phys. Rev. B 4, 187 (1971) 1. D. Gross and J.L. Olsen, Cryogenics 1, 91(1960) 13. E.F. Harris and D.E. Mapother, Phys. Rev. 165, 5 (1968) 14. C. Palmy et al., (1970). Reported in 9 15. R. Griessen and R. Ott, Phys.Lett. 36A, 113 (1971) 16. D.C.Wallace, Journ. Appl. Phys. 41, 5055 (1970) 17. N.E. Phillips, Phys. Rev. 114, 676 (1959) 18. N.B. Brandt and N.I. Ginzburg, Sov.Phys.-Usp 8, 0 (1965)