A. N. Jadhav 1. Yeshwant Mahavidyalaya, Nanded. Maharashtra, India.

Similar documents
CONTRIBUTION FUNCTION OF MOLYBDENUM ATOM AND IONS IN ASTROPHYSICAL AND LABORATORY PLASMA AS A FUNCTION OF ELECTRON TEMPERATURE

Journal of Advances in Applied Sciences and Technology (2015) Vol. 2 Issue 2-3 Page 27-33

EXCITATION RATE COEFFICIENTS OF MOLYBDENUM ATOM AND IONS IN ASTROPHYSICAL PLASMA AS A FUNCTION OF ELECTRON TEMPERATURE

Electron temperature is the temperature that describes, through Maxwell's law, the kinetic energy distribution of the free electrons.

Plasma Spectroscopy Inferences from Line Emission

Effect of small amounts of hydrogen added to argon glow discharges: Hybrid Monte Carlo fluid model

Modeling Non-Equilbirum Plasma. Adam Foster

Theory of Gas Discharge

Thermal Equilibrium in Nebulae 1. For an ionized nebula under steady conditions, heating and cooling processes that in

Theory of optically thin emission line spectroscopy

International Atomic Energy Agency, Vienna, Austria. Charge Transfer in Collisions of Ions with atoms and molecules.

Plasma collisions and conductivity

7. Non-LTE basic concepts

Physics of heavy multiply-charged ions: Studies on the borderile of atomic and nuclear physics

Analysis of recombination and relaxation of non-equilibrium air plasma generated by short time energetic electron and photon beams

Photoionized Gas Ionization Equilibrium

PHYSICS OF THE SPACE ENVIRONMENT

LECTURE NOTES. Ay/Ge 132 ATOMIC AND MOLECULAR PROCESSES IN ASTRONOMY AND PLANETARY SCIENCE. Geoffrey A. Blake. Fall term 2016 Caltech

CHAPTER 22. Astrophysical Gases

LECTURE 23 SPECTROSCOPY AND ATOMIC MODELS. Instructor: Kazumi Tolich

Ay Fall 2004 Lecture 6 (given by Tony Travouillon)

The CHIANTI Atomic Database

Example: model a star using a two layer model: Radiation starts from the inner layer as blackbody radiation at temperature T in. T out.

Collisional Excitation and N-Level Atoms.

Auger & X-ray Fluorescence

Time-dependent kinetics model for a helium discharge plasma

Deriving the coronal hole electron temperature: electron density dependent ionization / recombination considerations

Collisions and transport phenomena

Very deep spectroscopy of planetary nebula NGC7009 The rich optical recombination spectrum and new effective recombination coefficients

Calculating Radiative Recombination Continuum From a Hot Plasma

Interstellar Astrophysics Summary notes: Part 2

GCR calculations for Magnesium, Argon, Iron and other elements A different ADAS approach

Photoionization Modelling of H II Region for Oxygen Ions

Fundamentals of Plasma Physics

Matti Laan Gas Discharge Laboratory University of Tartu ESTONIA

6. Stellar spectra. excitation and ionization, Saha s equation stellar spectral classification Balmer jump, H -

Notes on Photoionized Regions Wednesday, January 12, 2011

CHIANTI An atomic database for astrophysical plasmas

Diffusion during Plasma Formation

EXPERIMENT 14. The Franck-Hertz Experiment. E 1 E 2 = hf (1)

Processes and Diagnostics in Collisional Plasmas

Reactive Collisions of Electrons with H 2. cations and isotopologues : Computations and comparison with measurements

7. Non-LTE basic concepts

Physics and Chemistry of the Interstellar Medium

Internal conversion electrons and SN light curves

Spectral Line Shapes. Line Contributions

Neutron Interactions Part I. Rebecca M. Howell, Ph.D. Radiation Physics Y2.5321

Study of Electron Energy and Angular Distributions and Calculations of X-ray, EUV Line Flux and Rise Times

Lasers PH 645/ OSE 645/ EE 613 Summer 2010 Section 1: T/Th 2:45-4:45 PM Engineering Building 240

Stellar Astrophysics: The Classification of Stellar Spectra

Production of HCI with an electron beam ion trap

AGN Physics of the Ionized Gas Physical conditions in the NLR Physical conditions in the BLR LINERs Emission-Line Diagnostics High-Energy Effects

Collisional-Radiative Model of Molecular Hydrogen

Astrophysics of Gaseous Nebulae and Active Galactic Nuclei

Electromagnetic Spectra. AST443, Lecture 13 Stanimir Metchev

Today, I will present the first of two lectures on neutron interactions.

Isotopic yields from supernova light curves

Spring 2018 PTYS 510A

Planetary Atmospheres

ANALYTICAL SCIENCES MAY 2016, VOL The Japan Society for Analytical Chemistry

Interactions of Particulate Radiation with Matter. Purpose. Importance of particulate interactions

ATOMS. Central field model (4 quantum numbers + Pauli exclusion) n = 1, 2, 3,... 0 l n 1 (0, 1, 2, 3 s, p, d, f) m l l, m s = ±1/2

Lasers PH 645/ OSE 645/ EE 613 Summer 2010 Section 1: T/Th 2:45-4:45 PM Engineering Building 240

Plasma Physics Prof. Vijayshri School of Sciences, IGNOU. Lecture No. # 38 Diffusion in Plasmas

Lecture 14 (11/1/06) Charged-Particle Interactions: Stopping Power, Collisions and Ionization

Radiative Properties of Krypton Plasma & Emission of Krypton DPP Source in Water-Window Spectral Range

Estimating the plasma flow in a recombining plasma from

6. Stellar spectra. excitation and ionization, Saha s equation stellar spectral classification Balmer jump, H -

Chapter 3. Collision processes. 3.1 Electron impact ionization

24/ Rayleigh and Raman scattering. Stokes and anti-stokes lines. Rotational Raman spectroscopy. Polarizability ellipsoid. Selection rules.

Emitted Spectrum Summary of emission processes Emissivities for emission lines: - Collisionally excited lines - Recombination cascades Emissivities

Joint ICTP-IAEA Workshop on Fusion Plasma Modelling using Atomic and Molecular Data January 2012

X-ray Radiation, Absorption, and Scattering

In this block the two transport mechanisms will be discussed: diffusion and drift.

Radiative-collisional processes in electron-tungsten ions collisions: quasiclassical calculations and data

SOLID STATE PHYSICS. Second Edition. John Wiley & Sons. J. R. Hook H. E. Hall. Department of Physics, University of Manchester

Fundamental Stellar Parameters. Radiative Transfer. Stellar Atmospheres. Equations of Stellar Structure

16.55 Ionized Gases Problem Set #5

6. Stellar spectra. excitation and ionization, Saha s equation stellar spectral classification Balmer jump, H -

Cold Clouds in Cool Cores

Chapter V: Interactions of neutrons with matter

Effect of iron ionization balance on X-ray spectral analysis

ASTR-1010: Astronomy I Course Notes Section IV

Some fundamentals. Statistical mechanics. The non-equilibrium ISM. = g u

LINE INTENSITY RATIOS IN THE EIS RANGE SENSITIVE TO ELECTRON DENSITIES IN 10 7 K PLASMAS

arxiv: v1 [astro-ph.sr] 14 May 2010

Collisional radiative model

Chapter 44. Nuclear Structure

Collisional-Radiative Models and the Emission of Light

Atomic Transitions II & Molecular Structure

Emissivity: A Program for Atomic Emissivity Calculations

Chapter Three (Nuclear Radiation)

CMFGEN. Associate every atomic species with a given identification number

Spectral analysis of K-shell X-ray emission of magnesium plasma produced by ultrashort high-intensity laser pulse irradiation

Cold Metastable Neon Atoms Towards Degenerated Ne*- Ensembles

3. Stellar Atmospheres: Opacities

Combinatorial RF Magnetron Sputtering for Rapid Materials Discovery: Methodology and Applications

Lecture Outline: Spectroscopy (Ch. 4)

X-ray spectroscopy of nearby galactic nuclear regions

The Non Equilibrium Ionization Model in ISIS

Transcription:

Departure from Maxwellian Velocity Distribution of High Temperature Plasma in Solar Flares where Almost All Electrons have been Stripped out from Iron Atoms A. N. Jadhav 1 1 Department of Electronics, Yeshwant Mahavidyalaya, Nanded. Maharashtra, India. Email: angadjadhav2007@rediffmail.com Abstract The spectral line intensity is proportional to the contribution function. The Contribution function can be found by taking product of fractional ion abundance and its excitation rate coefficient of upper state of transition emitting the spectral line in consideration. In present work the fractional abundance, excitation rate coefficient and Contribution function of Fe XXV ( = 1.85 A o ) and Fe XXVI ( = 1.79 A 0 ) as a function of Electron Temperature are computed and presented graphically. The contribution function of these ions is compared with their observed contribution function. The electron temperature for computed contribution function values are found slightly greater compared to values of the electron temperature corresponding to values of observed contribution function due to departure from maxwellian velocity distribution in a high temperature plasma in solar flares where almost all electrons of Iron have been stripped out. Keywords: Solar flares, excitation Rate Coefficient, fractional Abundance, contribution function, Electron Temperature. Subject Classification: Plasma 1. Introduction It is well known that energy states of atoms and ions in the plasma are populated by electron collisions and depopulated by collisions of ions with slow electrons. Besides the collisional processes the atomic and ionic states are populated and depopulated due to some radiative processes also. Electrons passing through the plasma transfer their energy to the plasma particles by two types of collisions i) Elastic collisions ii) Inelastic collisions. In elastic collisions the transfer of kinetic energy of electron in to the kinetic energy of the plasma particles (atoms or ions) takes place. In this process the kinetic energy of the Dr. A. N.Jadhav 1 Page 131

colliding particles is conserved. This type of collisional process is responsible to the heating of the plasma particles to some extent. In fact the second type of collision i.e. inelastic collisions are mainly responsible for the excitation of atoms and ions in the plasma. Any collision in which the internal energy of excitation of a particle is changed is referred to as inelastic collision. In this type of collision the kinetic energy of electron is converted into potential energy of colliding plasma particles and the plasma particles get excited. These particles in excited states either transfer their energy back to the electron or they undergo a transition giving radiative emission. The rate of transfer of energy from the electrons to the plasma particles may be written as, de N C N E N N C E N N C E dt (1) g e e c gi e in j gi e dex i j j where, N g is number of gas particles. C e is coefficient of elastic collision. E c is energy transferred in elastic collisions. C in is rate coefficient of inelastic collisions. E j is energy of the j th state excited by elastic collision. C dex is de-excitation rate coefficient. E i is energy of excited particles which transfers its energy to the electrons. The sum runs over all possible energy states of the plasma particles. 2. Electron Impact Excitation (EIE) In electron impact excitation, the energy from the high energy electrons is transferred to the colliding atoms or ions in the plasma. When an electron having energy more than the excitation energy of an electron rotating around nucleus of an atom / ion collides with the atom / ion may transfer its energy to the system and this may result in excitation of the rotating electron to a higher orbit. The probability of excitation depends upon energy of exciting electron and cross section of excitation at that particular energy. The excitation rate depends upon the excitation cross section and the number of effective collisions made by the electron. The number of effective collisions is function of electron velocity, which intern is a function of electron temperature (T e ). As we know that the plasmas consists of atoms, ions and electrons, there can be two types of electron impact excitation processes depending upon whether the colliding particles are atoms in ground state or ion in ground state. And accordingly these electron impact excitation (EIE) rate coefficients are defined as direct excitation and stepwise excitation respectively. 2.1 Penning Excitation Excitation energy can be exchanged between neutral atoms. In particular, an excited atom can get ionized by virtue of its excitation energy, if the later is larger than the required ionization energy. Such a process is made more probable if the excited atom is in metastable state and has thus longer lifetime in which the particle may undergo an effective collision. When one of the colliding atoms is in metastable state and the other one is in ground state, Dr. A. N.Jadhav 1 Page 132

there is a probability of ionizing second atom and getting excited to the excited state depending upon the energy of the metastable atom. Such a process is referred to as penning excitation. 2.2 Duffenduck Excitation The process in which an ion having charge z in a ground state, when collide with the other ion having charge z' in ground state, transfers its energy to the colliding partner and the other ion gets ionized. This process of ionization and excitation of one ion and recombination of other ion is known as duffenduck excitation or charge transfer. 3. The Excitation Rate Coefficients Excitation Rate Coefficients are useful in computing the contribution functions of various spectral lines. In present work, to study the excitation rate coefficient of different ionic species of iron, we have computed excitation rate coefficient of iron ions Fe XXV and Fe XXVI using formulae used in [1] as a function of electron temperature and few amongst them are presented graphically in figure (1). Fig. 1: Excitation Rate Coefficient Of Fe XXV and Fe XXVI As A Function Of Electron Temperature. From all the graphs it observes that, the excitation rate coefficient (ERC) is very sensitive function of the electron temperature before it reaches its peak value but the variation of the function becomes very slow varying function of electron temperature near its saturation value. Dr. A. N.Jadhav 1 Page 133

4. Fractional Abundance Plasma consists of the electrons and the ions with different charges. The collision between the atoms, ions of different charges and electrons results in ionization. At the same time the ions may capture the electrons and results in formation of ions of lower charge. The ionization and Recombination processes compete each other so that the ionization rate and recombination rate reach, each to a certain value and equilibrium is attained. As long as the electron temperature is not changed the equilibrium remains in a particular state. A change in electron temperature results in changing the densities of ions and electrons. Thus densities of ions and electrons are completely dictated by the electron temperature. The plasma emission depends upon the fraction of total density of species remaining in a particular ionized state, the electron density and the electron temperature. The amount of the fraction of the total density of species remaining in a particular ionized state is called as fractional abundance of that ion. Equation for the time rate of change of population density of ion of charge z can be written as, dn dt z e z z z 1 z 1 z z z 1 z 1 n N S N S N N (2) where z takes all values between 0 and maximum charge on the ion. The ionization state of each element of atomic number z is controlled by electron impact ionization (including autoionization) from state z z +1 with total rate coefficient S z,z (cm 3 sec -1 ) and radiative plus dielectronic recombination z+1 z with rate coefficient S z,z+1 ( cm 3 sec -1 ) In steady state, the time rate of change of population density of ion of charge z will be zero. In steady state condition, where the time rate change of population density of ion of charge z will be zero, the equation (14) reduces to, N z S z = N z+1 z+1 (3) The population density ratio ( N z,z+1 /N z,z ) of two adjacent ion stages Z +(z+1) and Z +z can be derived by using steady state equation (3). Dr. A. N.Jadhav 1 Page 134

N N z 1 z S z (4) z 1 where S (z) is ionization rate coefficient of ion of charge z. z+1 is recombination rate coefficient of ion of charge z+1. N z and N z+1 are densities of ion with charge z and z+1 respectively. 4.1 Expression for Fractional Abundance Population density ratio ( N z, z+1 / N z,z ) can be evaluated in terms of S z and z+1, as the values of S z and z+1 are fully determined by the electron temperature. Therefore the fractional abundance and population density of any ion in the plasma depends only on the electron temperature. The equation for fractional abundance of a Fe XXV and Fe XXVI species in plasma is written by using equation (4) and the procedure followed by [2]. The fractional abundance of an ion of charge z can be written as, Nz Fz (5) N z' z' where F z is the fractional abundance of ion of charge z. and N z is the density of ion with charge z. The sum runs over all possible ionized states. To study the behaviour of Fractional abundance of Fe XXIII through Fe XXVI as a function of electron temperature, they are computed using equation (5) and are presented graphically in figure (2). Dr. A. N.Jadhav 1 Page 135

Fig. 2: Fractional Abundance Of Iron Ions As A Function Of Electron Temperature. 5. The Contribution Function The contribution function is an electron temperature dependent part of the flux emitted by a spectral line and it is a measure of spectral line intensity because, spectral line intensity is proportional to their contribution function. The contribution function can be defined as the product of fractional ion abundance and the excitation rate coefficient of the upper state of the transition emitting the spectral line in consideration [3]. The equation for contribution function can be written as, C(z) = N z R zu (6) Where N z is the fractional density of the ion of charge z and R zu is the electron impact excitation rate coefficient of the state u of ion of charge z. 6. The Results and Discussion The Contribution Function Of Fe XXV (λ = 1.85 A o ) as a function of electron temperature is computed and presented graphically in figure 3. The normalized curve of contribution function of Fe XXV (dotted curve) is compared with observed contribution function (solid curve) of it in figure (4). Both curves are in close agreement with each other. The electron temperature at which solid curve and dash dot curve reaches to peak is 5.909 x 10 7 o K and 6.383 x 10 7 o K respectively. But at such a very high electron temperature, all the electrons in the plasma may not have maxwellian velocity distribution. Some electrons may have nonmaxwellian velocity distribution. By assuming 10% of electrons have non-maxwellian velocity destribution and 90% electron have maxwellian velocity destribution, the contribution fucntion is computed and plotted as a function of electron temperature (dash dot curve) and is compared with observed contribution function (solid curve) in figure(5). If we observe these curves, it observe that, both curves shows very good agreement. The electron temperature at which solid curve and dash dot curve shows peak are 5.91x10 7 o K and 5.90 x 10 7 o K. Thus we can conclude that, in a plasma at high electron temperature where almost 24 electrons have been stripped out from iron, neither the electrons have maxwellian velocity distribution nor they have non-maxwellian velocity distribution, but the electrons have mixed velocity distribution. Figure (6) shows the computed contribution function of Fe XXV ( = 1.85 A 0 ) as a function of electron temperature. We have also compared the computed normalized curve of contribution function of Fe XXVI ( = 1.79 A 0 ) (dash dot curve) assuming all the electrons having maxwellian velocity distribution with its observed contribution function (solid curve) in figure (7). In figure (7), the electron temperature at which the solid curve and the dash dot curve shows peaks are 120.5 x 10 6 o K and 136.4 x 10 6 o K respectively. By assuming 10 % of electrons having non-maxwellian velocity distribution and 90 % of electron having maxwellian velocity distribution, we have computed contribution function for Fe XXVI ( = 1.79 A 0 ) and is plotted in figure (8) as a function of electron temperature (dash dot curve), Dr. A. N.Jadhav 1 Page 136

along with observed contribution function. Both curves shows close agreement with each other up to peak and have slight error after peak. Fig. 3 : Contribution Function ( Without Normalization ) Of Fe XXV ( = 1.85 A o ) As a Function of Electron Temperature. Fig. 4 : Normalized Curve ( Dotted Curve) For Contribution Function Of Fe XXV ( = 1.85 A o ) In Present Work Is Compared With Observed Contribution Function (Solid Curve) As A Function Of Electron Temperature. Dr. A. N.Jadhav 1 Page 137

Fig. 5: Normalized Curve (Dash Dot Curve) For Contribution Function Of Fe XXV ( = 1.8 5 A 0 ) With Mixed Maxwellian Velocity distribution In Present Work Is Compared With Observed Contribution Function (Solid Curve) As A Function Of Electron Temperature. Fig. 6: Contribution Function Of Fe XXVI ( = 1.79 A 0 ) (Without Normalization) As A Function Of Electron Temperature. Dr. A. N.Jadhav 1 Page 138

Fig. 7 : Normalized Curve (Dotted Curve) For Contribution Function of Fe XXVI ( = 1.79 A o ) In Present Work Is Compared With Observed Contribution Function (Solid Curve) As A Function Of Electron Temperature. Fig. 8: Normalized Curve (Dash Dot Curve) For Contribution function of Fe XXVI ( = 1.79 A 0 ) With Mixed Maxwellian Velocity distribution In Present Work Is Compared With Observed Contribution Function (Solid Curve) As A Function Of Electron Temperature. Dr. A. N.Jadhav 1 Page 139

7. Conclusion Plasma at high electron temperature where almost all electrons have been stripped out from iron, neither the electrons have maxwellian velocity distribution nor they have non-maxwellian velocity distribution, but the electrons have mixed velocity distribution. 8. References [1] C Breton, C. De Michelis and M. Mattioli " Ionisation equilibrium and radiative cooling of a high temperature plasma " J. Quantitative Spectroscopy 19, 367 (1978). [2] A N Jadhav, Fractional abundance of neutral atoms and ionic species of iron and molybdenum as a function of electron temperature in astrophysical and laboratory plasma, IJARBAS, Vol.2 Issue 1, (2015) pp 12-15. [3] G A Doschek, High Temperature Plasma in Solar Flares, E.O.H. Hulburt Centre for space Research, Naval Research Laboratory, Washinton, D. C. 20375-5000, U. S. A. Dr. A. N.Jadhav 1 Page 140