Kinetics of Solid-Gas Reactions and Their Application to Carbonate Looping Systems
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Rate Constants and Kinetic Isotope Effects for Methoxy Radical Reacting with NO2 and O2 Jiajue Chai, Hongyi Hu, Theodore
Rate Constants and Kinetic Isotope Effects for Methoxy Radical Reacting with NO2 and O2 Jiajue Chai, Hongyi Hu, Theodore. S. Dibble* Department of Chemistry, College of Environmental Science and Forestry, State University of New York, Syracuse, New York 13210, United States Geoffrey. S. Tyndall,* and John. J. Orlando Atmospheric Chemistry Division, National Center for Atmospheric Research, Boulder, Colorado 80307, United States Abstract Relative rate studies were carried out to determine the temperature dependent rate constant ratio k1/k2a: CH3O• + O2 → HCHO + HO2• (R1) CH3O• + NO2 (+M) → CH3ONO2 (+ M) (R2a) over the temperature range 250-333 K in an environmental chamber at 700 Torr using FTIR detection. Absolute rate constants k2 were determined using laser flash photolysis/laser induced fluorescence under the same conditions. The analogous experiments were carried out for the reactions of perdeuterated methoxy radical (CD3O•). Absolute rate constants k2 were in excellent agreement with the recommendations of the JPL Data Evaluation panel. The combined data (i.e., 3 -1 k1/k2 and k2) allow determination of k1 as cm s , corresponding to 1.4 × 10-15 cm3 s-1 at 298 K. The rate constant at 298 K is in excellent agreement with previous work, but the observed temperature dependence is less than previously reported. The deuterium isotope effect, kH/kD, can be expressed in Arrhenius form as The deuterium isotope effect does not appear to be greatly influenced by tunneling, which is consistent with previous theoretical work by Hu and Dibble (Hu, H.; Dibble, T. S., J. Phys. Chem. A 2013, 117, 14230–14242). Keywords: methylnitrite, formaldehyde, methylnitrate, alkoxy radicals, kinetic isotope effect * [email protected], [email protected] 1 I. -
Schlieren Imaging of Loud Sounds and Weak Shock Waves in Air Near the Limit of Visibility
Shock Waves DOI 10.1007/s00193-009-0226-6 ORIGINAL ARTICLE Schlieren imaging of loud sounds and weak shock waves in air near the limit of visibility Michael John Hargather · Gary S. Settles · Matthew J. Madalis Received: 27 April 2009 / Accepted: 4 August 2009 © Springer-Verlag 2009 Abstract A large schlieren system with exceptional sensi- Keywords Shock waves · Nonlinear acoustics · Sound · tivity and a high-speed digital camera are used to visualize Noise · Schlieren · High-speed imaging loud sounds and a variety of common phenomena that pro- duce weak shock waves in the atmosphere. Frame rates var- PACS 42.79.Mt · 43.25.+y ied from 10,000 to 30,000frames/s with microsecond frame exposures. Sound waves become visible to this instrumenta- tion at frequencies above 10kHz and sound pressure levels 1 Introduction in the 110dB (6.3Pa) range and above. The density gradient produced by a weak shock wave is examined and found to Visualizing sound-wave motion in air has been a dream of sci- depend upon the profile and thickness of the shock as well as entists and engineers for at least a century and a half, although the density difference across it. Schlieren visualizations of sound waves and weak shock waves were initially confused. weak shock waves from common phenomena include loud August Toepler’s (1836–1912) epitaph, “He was the first to trumpet notes, various impact phenomena that compress a see sound,” actually referred to his schlieren imaging of weak bubble of air, bursting a toy balloon, popping a champagne shock waves from electric sparks [1]. -
Gas Kinetics in Galactic Disk. Why We Do Not Need a Dark Matter to Explain Rotation Curves of Spirals? Anton Lipovka
Gas kinetics in galactic disk. Why we do not need a dark matter to explain rotation curves of spirals? Anton Lipovka To cite this version: Anton Lipovka. Gas kinetics in galactic disk. Why we do not need a dark matter to explain rotation curves of spirals?. 2018. hal-01832309v3 HAL Id: hal-01832309 https://hal.archives-ouvertes.fr/hal-01832309v3 Preprint submitted on 24 Jul 2020 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Gas kinetics in galactic disk. Why we do not need a dark matter to explain rotation curves of spirals? Lipovka A.A. Department of Research for Physics, Sonora University, 83000, Hermosillo, Sonora, México May 27, 2020 Abstract In present paper, we analyze how the physical properties of gas affect the Rotation Curve (RC) of a spiral galaxy. It is shown, that the observed non-Keplerian RCs measured for outer part of disks, and the observed radial gas distribution are closely related by the diffusion equation, which clearly indicates that no additional mass (Dark Matter) is need. It is stressed, that while the inner part of the RC is subject of the Kepler law, for the correct description of the outer part of the RC, the collisional property of the gas should also be taken into account. -
Tables of Rate Constants for Gas Phase Chemical Reactions of Sulfur Compounds (1971-1979)
NBSIR 80-2118 Tables of Rate Constants for Gas Phase Chemical Reactions of Sulfur Compounds (1971-1979) Francis Westley Chemical Kinetics Division Center for Thermodynamics and Molecular Science National Measurement Laboratory National Bureau of Standards U.S. Department of Commerce Washington. D.C. 20234 July 1980 Interim Report Prepared for Morgantown Energy Technology Center Department of Energy Morgantown, West Virginia 26505 Fice of Standard Reference Data itional Bureau of Standards ashington, D.C. 20234 c, 2 Jl 1 m * rational bureau 07 STANDARDS LIBRARY NBSIR 80-2118 wov 2 4 1980 TABLES OF RATE CONSTANTS FOR GAS f)Oi Clcc -Ore PHASE CHEMICAL REACTIONS OF SULFUR COMPOUNDS (1971-1979) 1 5 (o lo-z im Francis Westley Chemical Kinetics Division Center for Thermodynamics and Molecular Science National Measurement Laboratory National Bureau of Standards U.S. Department of Commerce Washington, D.C. 20234 July 1980 Interim Report Prepared for Morgantown Energy Technology Center Department of Energy Morgantown, West Virginia 26505 and Office of Standard Reference Data National Bureau of Standards Washington, D.C. 20234 U.S. DEPARTMENT OF COMMERCE, Philip M. Klutznick, Secretary Luther H. Hodges, Jr., Deputy Secretary Jordan J. Baruch, Assistant Secretary for Productivity, Technology, and Innovation NATIONAL BUREAU OF STANDARDS. Ernest Ambler, Director . i:i : a 1* V'.OTf in. te- ?') t aa.‘ .1 J Table of Contents Abstract 1 Introduction 2 Guidelines for the User 4 Table of Arrhenius Parameters for Chemical Reactions of Sulfur Compounds 12 Reactions of: S(Sulfur atom) 12 $2(Sulfur dimer) 20 S0(Sulfur monoxide) 21 S02(Sulfur dioxide 23 S0 (Sulfur trioxide) 28 3 S20(Sul fur oxide^O) ) 29 SH (Mercapto free radical) 29 H2S (Hydroqen sulfide 31 CS (Carbon monosulfide free radical) 32 CS2 (Carbon disulfide) 33 COS (Carbon oxide sulfide) 35 CH^S* ( Methyl thio free radical) 36 CH^SH (Methanethiol ) 36 cy-CF^CF^S (Thiirane) 37 CH^SCF^* (Methyl, (methyl thio)-, free radical) ... -
Classical and Modern Methods in Reaction Rate Theory
J. Phys. Chem. 1988, 92, 3711-3725 3711 loss associated with the transition between states is offset by a For the Re( MQ+)-based complexes an additional complication gain in energy in the intramolecular vibrations (eq 3). to intramolecular electron transfer exists arising from a "flattening" On the other hand, if (AGe,,2 + A0,2) > (AG,,l + A,,,) (Figure of the relative orientations of the two rings of the MQ+ ligand 4B) and nuclear tunneling effects in the librational modes are when it accepts an However, the analysis presented unimportant, intramolecular electron transfer can not occur in here does provide a general explanation for the role of free energy a frozen environment. The situation is the same as in Figure 3A. change in environments where dipole motions are restricted. For Even direct Re(1) - MQ' excitation (process a in Figure 4B) a directed, intramolecular electron transfer such as reaction 1, must either lead to the ground state by emission or to the Re- the change in electronic distribution between states will, in general, (11)-bpy'--based MLCT state by reverse electron transfer: lead to a difference between Ao,l and A0,2. This difference creates a solvent dipole barrier to intramolecular electron transfer. It [ (bpy)Re"(CO) 3( MQ')] 2+* -+ (bpy'-)Re"( CO) 3(MQ')] 2'* follows from eq 4 that if light-induced electron transfer is to occur (5) in a frozen environment, the difference in solvent reorganizational The inversion in the sense of the electron transfer in the frozen energy, A& = bS2- A,,, must be compensated for by a favorable environment is induced energetically by the greater solvent re- free energy change, A(AG) = - AGes,l,as organizational energy for the lower excited state, A0,2 > Ao,l - Aces,~- AGes.2 > Ao-2 - &,I (AGes,2 - AGes,l)* or In a macroscopic sample, a distribution of solvent dipole en- vironments exists around the assembly of ground states. -
Eyring Activation Energy Analysis of Acetic Anhydride Hydrolysis in Acetonitrile Cosolvent Systems Nathan Mitchell East Tennessee State University
East Tennessee State University Digital Commons @ East Tennessee State University Electronic Theses and Dissertations Student Works 5-2018 Eyring Activation Energy Analysis of Acetic Anhydride Hydrolysis in Acetonitrile Cosolvent Systems Nathan Mitchell East Tennessee State University Follow this and additional works at: https://dc.etsu.edu/etd Part of the Analytical Chemistry Commons Recommended Citation Mitchell, Nathan, "Eyring Activation Energy Analysis of Acetic Anhydride Hydrolysis in Acetonitrile Cosolvent Systems" (2018). Electronic Theses and Dissertations. Paper 3430. https://dc.etsu.edu/etd/3430 This Thesis - Open Access is brought to you for free and open access by the Student Works at Digital Commons @ East Tennessee State University. It has been accepted for inclusion in Electronic Theses and Dissertations by an authorized administrator of Digital Commons @ East Tennessee State University. For more information, please contact [email protected]. Eyring Activation Energy Analysis of Acetic Anhydride Hydrolysis in Acetonitrile Cosolvent Systems ________________________ A thesis presented to the faculty of the Department of Chemistry East Tennessee State University In partial fulfillment of the requirements for the degree Master of Science in Chemistry ______________________ by Nathan Mitchell May 2018 _____________________ Dr. Dane Scott, Chair Dr. Greg Bishop Dr. Marina Roginskaya Keywords: Thermodynamic Analysis, Hydrolysis, Linear Solvent Energy Relationships, Cosolvent Systems, Acetonitrile ABSTRACT Eyring Activation Energy Analysis of Acetic Anhydride Hydrolysis in Acetonitrile Cosolvent Systems by Nathan Mitchell Acetic anhydride hydrolysis in water is considered a standard reaction for investigating activation energy parameters using cosolvents. Hydrolysis in water/acetonitrile cosolvent is monitored by measuring pH vs. time at temperatures from 15.0 to 40.0 °C and mole fraction of water from 1 to 0.750. -
Project RAND Publication: RA-15022
, , ,-.. ,'. --. - ~.-~~ UNCLASSIFIED (rA) AERODYNAMICS, GAS DYNAMICS AND HEAT TRANSFER PROBLEMS OF A SATELLITE ROCKET RA-15022 February 1, 1947 UNCLASSI FI ED DOUGLAS AIRCRAFT COMPANY, INC. == DECLASSIFIED lAW E012958 BY EO Review Team DATE &' - ) r; --- :J-cJl r} This document contains information affecting the national defense of the United States within the meaning of the Espionage Act, SO U.S.C., 31 and 32, as amended. Its transmission or the revelation of its contents in any manner to an unauthorized person is prohibited by law. SECRET TABLE OF CONTENTS LIST OF FIGURES ...... , ......................................................... v SUMMARy .........................................................................vii LIST OF SyMBOLS ............................................................... ix I. AERODYNAMICS .............................................................. I A. Drag ....................................................................... l 1. The Drag Forces Exerted on a Supersonic Rocket ......................... 1 2. Approximations Used in the Drag Analysis ............................... 4 3. Methods Employed in Evaluating the Drag ................................ 6 4. The Optimum Shape for a Satellite Rocket ......... , ..................... 8 5. Rarefied Gas Dynamics (Superaerodynamics) ............................. 20 B. Aerodynamics of Stability and Control. .. , ..............•.... : ............. 20 L Control Manent ..................................... '............ , ...... 21 2. Body Moment .......................................................... -
Gas Phase Reaction Kinetics of Neutral Oxygen Species
National Bureau ot Standards Library, £01 Admin. Bldg. FEB 3 1969 A11102 mbQQb NSRDS-NBS 20 All 1021 46006 /NSflOS-MI? N6S-.UB-CW NBS PUBLICATIONS Gas Phase Reaction Kinetics Of Neutral Oxygen Species U.S. DEPARTMENT OF COMMERCE NATIONAL BUREAU OF STANDARDS National Standard Reference Data Series National Bureau of Standards National Standard Reference Data System, Plan of Operation, NSRDS-NBS 1 — 15 cents* Thermal Properties of Aqueous Uni-univalent Electrolytes, NSRDS-NBS 2 — 45 cents* Selected Tables of Atomic Spectra, Atomic Energy Levels and Multiplet Tables — Si II, Si III, Si IV, NSRDS-NBS 3, Section 1 — 35 cents* Selected Tables of Atomic Spectra, Atomic Energy Levels and Multiplet Tables — Si I, NSRDS-NBS 3, Section 2 — 20 cents* Atomic Transition Probabilities, Volume I, Hydrogen Through Neon, NSRDS-NBS 4 — $2.50* The Band Spectrum of Carbon Monoxide, NSRDS-NBS 5 — 70 cents* Tables of Molecular Vibrational Frequencies, Part 1, NSRDS-NBS 6 — 40 cents* High Temperature Properties and Decomposition of Inorganic Salts, Part 1, Sulfates, NSRDS-NBS 7-35 cents* Thermal Conductivity of Selected Materials, NSRDS-NBS 8 — 11.00* Tables of Bimolecular Gas Reactions, NSRDS-NBS 9 — $2.00* Selected Values of Electric Dipole Moments for Molecules in the Gas Phase, NSRDS- NBS 10-40 cents* Tables of Molecular Vibrational Frequencies, Part 2, NSRDS-NBS 11 — 30 cents* Tables for the Rigid Asymmetric Rotor: Transformation Coefficient for Symmetric to Asymmetric Bases and Expectation Values of P§, P|, and Pf, NSRDS-NBS 12 — 60 cents* Hydrogenation -
Empirical Chemical Kinetics
Empirical Chemical Kinetics time dependence of reactant and product concentrations e.g. for A + 2B → 3C + D d[A] 1 d[B] 1 d[C] d[D] rate =− =− = = d2d3ddtttt =ν In general, a chemical equation is 0∑ ii R i nt()− n (0 ) The extent of a reaction (the advancement) = ii ν i For an infinitesmal advancement dξ each reactant/product =ν ξ concentration changes by d[Ri ]i d . d1d[R]ξ By definition, the rate == i ν ddtti Reaction rates usually depend on reactant concentrations, e.g., rate= k [A]xy [B] order in B total order = x+y rate constant In elementary reaction steps the orders are always integral, but they may not be so in multi-step reactions. The molecularity is the number of molecules in a reaction step. Rate Laws d[A] Zero order: −=k dt 0 [A] = [A]00 -[A]t kt [A]0 t1 = 2 2k 0 0 t −=d[A] First order: k1[A] [A] ln[A] dt − = kt1 [A]t [A]0 e ln 2 0 t 0 t t1 = 2 k1 d[A] 2 Second order: −=2[A]k [A] dt 2 [A] [A] = 0 t + 12[A]kt20 0 t -1=+ -1 [A]t [A]02 2kt 1 t1 = 2 2[A]k20 [A]-1 0 t Second-order Kinetics: Two Reactants A + B k → products da rate=− =kab a = [A], b =[B] dt =− − ka()()00 x b x ddxa Since aa=− x, =− 0 ddtt dx So =−ka()() x b − x dt 00 x dx kt = ∫ ()()−− 0 axbx00 −111x =−dx ()−−−∫ ()() ab000 ax 0 bx 0 −1 ab = ln 0 ()− ab00 ab 0 or more usefully, aa=+−0 ln ln ()abkt00 bb0 Data Analysis “Classical” methods of data analysis are often useful to explore the order of reactions, or to display the results (e.g. -
Kinetics and Atmospheric Chemistry
12/9/2017 Kinetics and Atmospheric Chemistry Edward Dunlea, Jose-Luis Jimenez Atmospheric Chemistry CHEM-5151/ATOC-5151 Required reading: Finlayson-Pitts and Pitts Chapter 5 Recommended reading: Jacob, Chapter 9 Other reading: Seinfeld and Pandis 3.5 General Outline of Next 3 Lectures • Intro = General introduction – Quick review of thermodynamics • Finlayson-Pitts & Pitts, Chapter 5 A. Fundamental Principles of Gas-Phase Kinetics B. Laboratory Techniques for Determining Absolute Rate Constants for Gas-Phase Reactions C. Laboratory Techniques for Determining Relative Rate Constants for Gas-Phase Reactions D. Reactions in Solution E. Laboratory Techniques for Studying Heterogeneous Reactions F. Compilations of Kinetic Data for Atmospheric Reactions 1 12/9/2017 Kinetics and Atmospheric Chemistry • What we’re doing here… – Photochemistry already covered – We will cover gas phase kinetics and heterogeneous reactions – Introductions to a few techniques used for measuring kinetic parameters • What kind of information do we hope to get out of “atmospheric kinetics”? – Predictive ability over species emitted into atmosphere • Which reactions will actually proceed to products? • Which products will they form? • How long will emitted species remain before they react? Competition with photolysis, wash out, etc. • Pare down list of thousands of possible reactions to the ones that really matter – Aiming towards idea practical predictive abilities • Use look up tables to decide if reaction is likely to proceed and determine an “atmospheric lifetime” -
Gas Kinetics Introduction
Gas Kinetics Introduction • Most deposition techniques rely on gas flow in a vacuum. • We need a model for understanding; – the speed and energy of the gas molecules as a function of temperature and pressure, – how these molecules interact with each other and their surroundings, – and how mass, heat and momentum is transported by these molecules. The Size of a Molecule (a very rough calculation) • Take water (liquid H2 O) as an example. • Oxygen has 8 protons and 8 neutrons for a total of 16 nucleons and Hydrogen has 1 proton. So water has 16+1+1=18 nucleons −24 m≈PN1 m . ≈ 66 × 10g −23 m18HO= mN 2 = . 99 × g 10 2 d HO2 N1= m 3 = . 35 ×22 molecules 10 / g HO2 HO2 ρ 1= .g 00 cm3 / HO2 1 V = 2= . 99 × −23 10cm 3 molecule / HO2 ρ N HOHO2 2 3 d=2 ×3 V5 . = 64− ×8 10cm HO2 4 HO2 The Distance Between Molecules in a Gas • Now take water vapor (gaseous H2 O). ρ 0= . 8 ×g 10−3 cm3 / HO2 1 −20 3 l V = 3= . 73 × 10cm molecule / HO2 HO2 ρ N HOHO2 2 l=3 V3 . = 34 ×−7 10cm HO2 HO2 l≈ 6 d HO2 HO2 Molecular Velocities • Basic assumptions: – We’ll assume an ideal gas where the gas molecules interact elastically (collisions are similar to the collisions of hard billiard balls). – The distance between molecules are large compared to their sizes. – There are no attractive or repulsive forces between the molecules and each molecule moves independently of the others. Maxwell-Boltzmann Distribution • Under these assumptions, the molecules of a gas have velocities that are distributed according to: 1 dn M ⎛ Mv2 ⎞ where f is the fractional number of 2 ⎜ ⎟ molecules, v is the velocity, M is the f() v= =4πv exp⎜− ⎟ molecular weight, T is the temperature n dv 2πRT ⎝ 2RT ⎠ and R is the universal gas constant. -
Mathematical Modeling of the Shockless Explosion Combustion
Dissertation Mathematical Modeling of the Shockless Explosion Combustion Phillip Berndt im August 2016 eingereicht am Fachbereich Mathematik und Informatik Freie Universität Berlin zur Erlangung des Grades eines Doktors der Naturwissenschaften Erstgutachter & Betreuer: Prof. Dr.-Ing. Rupert Klein Zweitgutachter: Prof. Dr.-Ing. Christian Oliver Paschereit Drittgutachter: Prof. Dr. rer.nat. Volker John Tag der Disputation: 02. Dezember 2016 Contents 1. Introduction 1 1.1. The Shockless Explosion Combustion . .4 1.2. The Reactive Euler Equations of Fluid Dynamics . .7 1.2.1. The One-Dimensional Reactive Euler Equations . .8 1.2.2. Ignition Delay Time and Excitation Time . 11 1.2.3. Lagrangian Picture . 13 1.2.4. Quasi One-Dimensional Flow . 16 2. Fuel Requirements and Blend Selection 19 2.1. Model Reduction for SEC Fuels . 20 2.2. Model for Idealized SEC Fuels . 24 2.2.1. Single-Stage Model . 25 2.2.2. Two-Stage Extension . 27 2.3. Fuel Selection for the Atmospheric SEC Test Rig . 29 2.4. Numerical Methods for the Simulation of Chemical Kinetics . 32 2.5. Intermediate Conclusion . 35 3. Numerical Methods for Multi-Species Gaseous Flow 37 3.1. Solution of the Riemann Problem for Ideal Gases . 38 3.1.1. Linearization of the Equations . 38 3.1.2. Primitive Form of the Equations . 39 3.1.3. Riemann Invariants . 40 3.1.4. Solution Strategy . 42 3.2. The HLLE Solver in Multi-Species Simulations . 43 3.2.1. Positivity . 44 3.2.2. Pressure Oscillations at Contact Discontinuities . 46 3.2.3. A Note on Larrouturou’s Positivity Correction . 49 3.3.