Detonation Structure
|
|
- Derek Chester Palmer
- 5 years ago
- Views:
Transcription
1 Planar Detonations and Detonation Structure Jerry Seitzman. 5 Mole Fraction.5..5 CH4 HO HCO emerature Methane Flame...3 Distance (cm) 5 5 emerature (K) Detonations - Coyright 4-5 by Jerry M. Seitzman. All rights reserved. ZND Model: Detonation Structure Generally, molecular collisions that euilibrate and translational energy recede chemical reactions characteristic momentum transfer collision < ns characteristic chemical reactions > O( µs) Suggests detonation is Zeldovich, von Neumann, Döring u leading shock followed u by reaction zone shock raises and M goes subsonic autoignition after delay heat release,, like deflagration shock reaction zone induction zone Detonations - Coyright 4-5 by Jerry M. Seitzman. All rights reserved.
2 Weak Detonations After leading shock wave, flow reduced to subsonic o achieve weak detonation, flow must reaccelerate to M > If induction/reaction zones only have heat release would violate nd Law M > can t go from subsonic to suersonic D flow with heat addition (> always drives toward M=) a M b < M > b Detonations -3 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. Weak Detonations Look at ath on Rayleigh Hugoniot a b c d e e a / o go from d to e, need negative heat release (endothermic reactions) reuires chemistry to overshoot euilibrium b,c d / Detonations -4 Coyright 4-5 by Jerry M. Seitzman. All rights reserved.
3 Chaman-Jouget Detonations No weak (unallowed), strong (unstable) detonation a b c d U a / Only leaves Chaman-Jouget solution C-J detonation is lanar detonation solution We have constraint to add to 5 conservation and state euations: M = 6 es., 6 unknowns! b,c d U / Detonations -5 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. CJ Detonation Euations Find detonation wave seed, D u and roduct roerties ( /, /, /, u ) CJ constraint u = a R Mass D = u = γ W Rayleigh γ + D = γ M = For strong detonation, / >> ( γ, W ) γ R W = D, γ + γ = + = + γ γ γ Detonations -6 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. 3
4 Detonations -7 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. CJ Detonation Euations W Virial, P.G. = W In above euations, still need roduct comosition to get γ, W and high, assume roducts in chem. euilibrium small changes in radical oulations/ollutants will not change roduct roerties significantly Hugoniot ( ) h h = + R e ( ) e = γ γ W a sol n method: guess, ; find Y i / D, / :Iterate Eamle: H -Air CJ Detonation 98 K, atm 5 5 Velocity (m/s) 5 5 M u D 4 3 u -u φ= Hydrogen (%) Detonation Mach # Detonations -8 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. 4
5 Detonation Limits 98 K, atm Don t get steady, selfsustained detonation if miture is too rich or too lean Not euil. issue kinetics, losses Detonations -9 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. Velocity (m/s) M u 5 D 4 3 u -u φ= Hydrogen (%) Detonation Mach # 3D Detonation Structure -d detonation -d/3-d detonation Detonations - Coyright 4-5 by Jerry M. Seitzman. All rights reserved. from immes et al., Astrohysical J., () 5
6 Front Proagation Detonations - Coyright 4-5 by Jerry M. Seitzman. All rights reserved. from immes et al., Astrohysical J., () Eerimental Evidence Smoke foil records trile oint tracks 4 mm Detonations - Coyright 4-5 by Jerry M. Seitzman. All rights reserved. 34 mm 6
7 rile Point Region Detonations -3 Coyright 4-5 by Jerry M. Seitzman. All rights reserved. from Numerical Simulations of Gaseous Detonations, 7
Cellular structure of detonation wave in hydrogen-methane-air mixtures
Open Access Journal Journal of Power Technologies 91 (3) (2011) 130 135 journal homepage:papers.itc.pw.edu.pl Cellular structure of detonation wave in hydrogen-methane-air mixtures Rafał Porowski, Andrzej
More informationChemical inhibiting of hydrogen-air detonations Sergey M. Frolov
Chemical inhibiting of hydrogen-air detonations Sergey M. Frolov Semenov Institute of Chemical Physics Moscow, Russia Outline Introduction Theoretical studies Classical 1D approach (ZND-model) Detailed
More informationDetonation of Gas Particle Flow
2 Detonation of Gas Particle Flow F. Zhang 2.1 Introduction Fine organic or metallic particles suspended in an oxidizing or combustible gas form a reactive particle gas mixture. Explosion pressures in
More informationAME 513. " Lecture 8 Premixed flames I: Propagation rates
AME 53 Principles of Combustion " Lecture 8 Premixed flames I: Propagation rates Outline" Rankine-Hugoniot relations Hugoniot curves Rayleigh lines Families of solutions Detonations Chapman-Jouget Others
More informationLecture 7 Detonation Waves
Lecture 7 etonation Waves p strong detonation weak detonation weak deflagration strong deflagration / 0 v =/ University of Illinois at Urbana- Champaign eflagrations produce heat Thermal di usivity th
More informationChemical Kinetics: NOx Mechanisms
Mole Fraction Temperature (K) Chemical Kinetics: Nx Mechanisms Jerry Seitzman. 5.15.1.5 CH4 H HC x 1 Temperature Methane Flame.1..3 Distance (cm) 15 1 5 KineticsNx -1 Nx Formation Already pointed out that
More informationAA210A Fundamentals of Compressible Flow. Chapter 13 - Unsteady Waves in Compressible Flow
AA210A Fundamentals of Compressible Flow Chapter 13 - Unsteady Waves in Compressible Flow The Shock Tube - Wave Diagram 13.1 Equations for irrotational, homentropic, unsteady flow ρ t + x k ρ U i t (
More informationCombustion Behind Shock Waves
Paper 3F-29 Fall 23 Western States Section/Combustion Institute 1 Abstract Combustion Behind Shock Waves Sandeep Singh, Daniel Lieberman, and Joseph E. Shepherd 1 Graduate Aeronautical Laboratories, California
More informationUNIVERSITY OF CALGARY. Stability of Detonation Wave under Chain Branching Kinetics: Role of the Initiation Step. Michael Anthony Levy A THESIS
UNIVERSITY OF CALGARY Stability of Detonation Wave under Chain Branching Kinetics: Role of the Initiation Step by Michael Anthony Levy A THESIS SUBMITTED TO THE FACULTY OF GRADUATE STUDIES IN PARTIAL FULFILLMENT
More informationDETONATION HAZARD CLASSIFICATION BASED ON THE CRITICAL ORIFICE PLATE DIAMETER FOR DETONATION PROPAGATION
DETONATION HAZARD CLASSIFICATION BASED ON THE CRITICAL ORIFICE PLATE DIAMETER FOR DETONATION PROPAGATION by Mitchell Cross A thesis submitted to the Department of Mechanical and Materials Engineering In
More informationLaminar Premixed Flames: Flame Structure
Laminar Premixed Flames: Flame Structure Combustion Summer School 2018 Prof. Dr.-Ing. Heinz Pitsch Course Overview Part I: Fundamentals and Laminar Flames Introduction Fundamentals and mass balances of
More informationNUMERICAL SIMULATION OF UNSTEADY NORMAL DETONATION COMBUSTION AJJAY OMPRAKAS. Presented to the Faculty of the Graduate School of
NUMERICAL SIMULATION OF UNSTEADY NORMAL DETONATION COMBUSTION by AJJAY OMPRAKAS Presented to the Faculty of the Graduate School of The University of Texas at Arlington in Partial Fulfillment of the Requirements
More informationEVALUATION OF HYDROGEN, PROPANE AND METHANE-AIR DETONATIONS INSTABILITY AND DETONABILITY
EVALUATION OF HYDROGEN, PROPANE AND METHANE-AIR DETONATIONS INSTABILITY AND DETONABILITY Borzou, B. 1 and Radulescu, M.I. 2 1 Mechanical Engineering Department, University of Ottawa, 161 Louis Pasteur,
More informationSteady, 1-d, constant area, adiabatic flow with no external work but with friction Conserved quantities
School of Aerosace Engineering Stead, -d, constant area, adiabatic flow with no external work but with friction Conserved quantities since adiabatic, no work: h o constant since Aconst: mass fluxρvconstant
More informationA second order scheme on staggered grids for detonation in gases
A second order scheme on staggered grids for detonation in gases Chady Zaza IRSN PSN-RES/SA2I/LIE August 1, 2016 HYP 2016, RWTH Aachen Joint work with Raphaèle Herbin, Jean-Claude Latché and Nicolas Therme
More informationTHERMODYNAMIC ANALYSIS OF COMBUSTION PROCESSES FOR PROPULSION SYSTEMS
2nd AIAA Aerospace Sciences Paper 2-33 Meeting and Exhibit January -8, 2, Reno, NV THERMODYNAMIC ANALYSIS OF COMBUSTION PROCESSES FOR PROPULSION SYSTEMS E. Wintenberger and J. E. Shepherd Graduate Aeronautical
More informationThe evolution and cellular structure of a detonation subsequent to a head-on interaction with a shock wave
Combustion and Flame 151 (2007) 573 580 www.elsevier.com/locate/combustflame The evolution and cellular structure of a detonation subsequent to a head-on interaction with a shock wave Barbara B. Botros
More informationINVESTIGATION OF INSTABILITIES AFFECTING DETONATIONS: IMPROVING THE RESOLUTION USING BLOCK-STRUCTURED ADAPTIVE MESH REFINEMENT PRASHAANTH RAVINDRAN
INVESTIGATION OF INSTABILITIES AFFECTING DETONATIONS: IMPROVING THE RESOLUTION USING BLOCK-STRUCTURED ADAPTIVE MESH REFINEMENT by PRASHAANTH RAVINDRAN Presented to the Faculty of the Graduate School of
More informationReacting Gas Mixtures
Reacting Gas Mixtures Reading Problems 15-1 15-7 15-21, 15-32, 15-51, 15-61, 15-74 15-83, 15-91, 15-93, 15-98 Introduction thermodynamic analysis of reactive mixtures is primarily an extension of the principles
More informationPresentation Start. Zero Carbon Energy Solutions 4/06/06 10/3/2013:; 1
Presentation Start 10/3/2013:; 1 4/06/06 What is an Explosion? Keller, J.O. President and CEO,, ISO TC 197, Technical Program Director for the Built Environment and Safety; Gresho, M. President, FP2FIRE,
More informationNUMERICAL AND THEORETICAL INVESTIGATIONS ON DETONATION- INERT CONFINEMENT INTERACTIONS
NUMERICAL AND THEORETICAL INVESTIGATIONS ON DETONATION- INERT CONFINEMENT INTERACTIONS Tariq D. Aslam and John B. Bdzil Los Alamos National Laboratory Los Alamos, NM 87545 hone: 1-55-667-1367, fax: 1-55-667-6372
More informationOn thermodynamic cycles for detonation engines
On thermodynamic cycles for detonation engines R. Vutthivithayarak, E.M. Braun, and F.K. Lu 1 Introduction Detonation engines are considered to potentially yield better performance than existing turbo-engines
More informationDetailed and Simplified Chemical Reaction Mechanisms for Detonation Simulation
Paper 05F- - Presented at the Fall 2005 Western States Section of the Combustion Institute, Stanford University, Oct. 17-1, 2005 Detailed and Simplified Chemical Reaction Mechanisms for Detonation Simulation
More informationDirect Simulation of Ultrafast Detonations in Mixtures
Direct Simulation of Ultrafast Detonations in Mixtures Patrick D. O Connor *, Lyle N. Long * and James B. Anderson * Department of Aerospace Engineering, The Pennsylvania State University, University Park,
More informationIgnition. Jerry Seitzman. Temperature (K) School of Aerospace Engineering Review. stable/steady self-sustained propagation of premixed flames
Mole Fraction Temperature (K) Ignition Jerry Seitzman 0. 500 0.5 000 0. 0.05 0 CH4 HO HCO x 000 Temperature Methane Flame 0 0. 0. 0. Distance (cm) 500 000 500 0 Ignition - Review So far, examined stable/steady
More informationSupersonic Combustion Simulation of Cavity-Stabilized Hydrocarbon Flames using Ethylene Reduced Kinetic Mechanism
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 9-12 July 2006, Sacramento, California AIAA 2006-5092 Supersonic Combustion Simulation of Cavity-Stabilized Hydrocarbon Flames using Ethylene
More informationTHRUST CHAMBER DYNAMICS AND PROPULSIVE PERFORMANCE OF AIRBREATHING PULSE DETONATION ENGINES
The Pennsylvania State University The Graduate School Department of Mechanical and Nuclear Engineering THRUST CHAMBER DYNAMICS AND PROPULSIVE PERFORMANCE OF AIRBREATHING PULSE DETONATION ENGINES A Thesis
More informationThe Dynamics of Detonation with WENO and Navier-Stokes Shock-Capturing
The Dynamics of Detonation with WENO and Navier-Stokes Shock-Capturing Christopher M. Romick, University of Notre Dame, Notre Dame, IN Tariq D. Aslam, Los Alamos National Laboratory, Los Alamos, NM and
More informationMild Ignition Phenomena in Rapid Compression Machines
25 th ICDERS August 2 7, 2015 Leeds, UK Kevin P. Grogan a, S. Scott Goldsborough b, Matthias Ihme a a Stanford University, Stanford, CA 94305 b Argonne National Laboratory, Argonne, IL 60439 1 Introduction
More informationChemistry Chapter 16. Reaction Energy
Chemistry Reaction Energy Section 16.1.I Thermochemistry Objectives Define temperature and state the units in which it is measured. Define heat and state its units. Perform specific-heat calculations.
More informationANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES
ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES V. Kopchenov*, S. Batura*, L. Bezgin*, N. Titova*, A. Starik* *CIAM, Russia Keywords:
More informationLecture 8 Laminar Diffusion Flames: Diffusion Flamelet Theory
Lecture 8 Laminar Diffusion Flames: Diffusion Flamelet Theory 8.-1 Systems, where fuel and oxidizer enter separately into the combustion chamber. Mixing takes place by convection and diffusion. Only where
More informationLawrence Livermore National. Laboratory. Adding Kinetics and Hydrodynamics to the CHEETAH Thermochemical Code UCRL-ID
Adding Kinetics and Hydrodynamics to the CHEETAH Thermochemical Code L. E. Fried, W. M. Howard, P. C. Souers, and L. Haselman January 15, 1997 This is an informal report intended primarily for internal
More informationTHERMODYNAMIC THEORY OF NON-IDEAL DETONATION AND FAILURE
THERMODYNAMIC THEORY O NON-IDEAL DETONATION AND AILURE W yers rown Mass Action Research Consultancy Devonshire House, 14 Corbar Road, uxton, SK17 6RQ, UK and Department of Chemistry University of Manchester,
More informationUNIVERSITY OF CINCINNATI
UNIVERSITY OF CINCINNATI Date: June 14,2005 I, Arun Prakash Raghupathy, hereby submit this work as part of the requirements for the degree of: Master of Science in: Mechanical Engineering It is entitled:
More informationFlame Acceleration and Transition to Detonation in Benzene-Air Mixtures
Flame Acceleration and Transition to Detonation in Benzene-Air Mixtures R. Knystautas, J.H.S. Lee Dept. of Mechanical Engineering McGill University, Montreal, Canada J. E. Shepherd Graduate Aeronautical
More informationVerified Calculation of Nonlinear Dynamics of Viscous Detonation
Verified Calculation of Nonlinear Dynamics of Viscous Detonation Christopher M. Romick, University of Notre Dame, Notre Dame, IN Tariq D. Aslam, Los Alamos National Laboratory, Los Alamos, NM and Joseph
More informationThe role of diffusion at shear layers in irregular detonations
The role of diffusion at shear layers in irregular detonations Marco Arienti 1 Joseph E. Shepherd 2 1 United Technologies Research Center, 411 Silver Lane, East Hartford, CT 06108 2 California Institute
More informationThe Deflagration Phase of Type Ia SNe
The Center for Astrophysical Thermonuclear Flashes The Deflagration Phase of Type Ia SNe Alan Calder ASC FLASH Center Type Ia Supernova Team Type Ia Supernovae and Cosmology August 5, 2004 An Advanced
More informationHydrocarbon - Air - Nitrous Oxide Detonations
Hydrocarbon - Air - Nitrous Oxide Detonations M. Kaneshige Mechanical Engineering R. Akbar, J.E. Shepherd Graduate Aeronautical Laboratories California Institute of Technology April 14-15, 1997 Western
More informationEFFECTS OF PRESSURE AND PREHEAT ON SUPER-ADIABATIC FLAME TEMPERATURES IN RICH PREMIXED METHANE/AIR FLAMES
Combust. Sci. and Tech., 180: 437 452, 2008 Copyright # Taylor & Francis Group, LLC ISSN: 0010-2202 print/1563-521x online DOI: 10.1080/00102200701741285 EFFECTS OF PRESSURE AND PREHEAT ON SUPER-ADIABATIC
More informationCarbon Science and Technology
ASI RESEARCH ARTICLE Carbon Science and Technology Received:10/03/2016, Accepted:15/04/2016 ------------------------------------------------------------------------------------------------------------------------------
More informationExperimental Observation of Fast Deflagrations and Transition to Detonations in Hydrogen-Air-Mixtures
Experimental Observation of Fast Deflagrations and Transition to Detonations in Hydrogen-Air-Mixtures A. Eder, C. Gerlach, F. Mayinger Lehrstuhl A für Thermodynamik Technische Universität München, Germany
More informationFundamentals of Rotating Detonation. Toshi Fujiwara (Nagoya University)
Fundamentals of Rotating Detonation Toshi Fujiwara (Nagoya University) New experimental results Cylindical channel D=140/150mm Hydrogen air; p o =1.0bar Professor Piotr Wolanski P [bar] 10 9 8 7 6 5 4
More informationIn order for two molecules to react, they must with each other. When they collide they transfer among themselves.
Chemistry 12 Reaction Kinetics II Name: Date: Block: 1. Collision Theory 2. Activation Energy 3. Potential Energy Diagrams Collision Theory (Kinetic Molecular Theory) In order for two molecules to react,
More informationChemistry 123: Physical and Organic Chemistry Topic 4: Gaseous Equilibrium
Topic 4: Introduction, Topic 4: Gaseous Equilibrium Text: Chapter 6 & 15 4.0 Brief review of Kinetic theory of gasses (Chapter 6) 4.1 Concept of dynamic equilibrium 4.2 General form & properties of equilbrium
More informationModule 3: Laminar Premixed Flames
Module 3: aminar Premixed Flames Objectives Scoe Reading Assignments Assignment Schedule Objectives By the end of this module, students should be able to: Define what is meant by Premixed Flame Understand
More informationINFLUENCE OF INITIAL DENSITY ON THE REACTION ZONE FOR STEADY-STATE DETONATION OF HIGH EXPLOSIVES
INFLUENCE OF INITIAL DENSITY ON THE REACTION ZONE FOR STEADY-STATE DETONATION OF HIGH EXPLOSIVES Alexander V. Utkin, Sergey A. Kolesnikov, Sergey V. Pershin, and Vladimir E. Fortov Institute of Problems
More informationAsymptotic Structure of Rich Methane-Air Flames
Asymptotic Structure of Rich Methane-Air Flames K. SESHADRI* Center for Energy and Combustion Research, Department of Mechanical and Aerospace Engineering, University of California at San Diego, La Jolla,
More informationHydrogen addition to the Andrussow process for HCN synthesis
Applied Catalysis A: General 201 (2000) 13 22 Hydrogen addition to the Andrussow process for HCN synthesis A.S. Bodke, D.A. Olschki, L.D. Schmidt Department of Chemical Engineering and Materials Science,
More informationDetonations in mixtures containing nitrous oxide
Issw22 Detonations in mixtures containing nitrous oxide M. Kaneshige, E. Schultz, U.J. Pfahl, J.E. Shepherd, R. Akbar Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena, CA
More informationSPC 407 Sheet 6 - Solution Compressible Flow Fanno Flow
SPC 407 Sheet 6 - Solution Comressible Flow Fanno Flow 1. What is the effect of friction on flow velocity in subsonic and suersonic Fanno flow? Friction increases the flow velocity in subsonic Fanno flow,
More informationAn analytical model for direct initiation of gaseous detonations
Issw21 An analytical model for direct initiation of gaseous detonations C.A. Eckett, J.J. Quirk, J.E. Shepherd Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena CA 91125,
More informationComputational analysis of re-ignition and re-initiation mechanisms of quenched detonation waves behind a backward facing step
Available online at www.sciencedirect.com ScienceDirect Proceedings of the Combustion Institute xxx (2014) xxx xxx Proceedings of the Combustion Institute www.elsevier.com/locate/proci Computational analysis
More informationModeling and Simulation of Plasma-Assisted Ignition and Combustion
Modeling and Simulation of Plasma-Assisted Ignition and Combustion Vigor Yang and Sharath Nagaraja Georgia Institute of Technology Atlanta, GA AFOSR MURI Fundamental Mechanisms, Predictive Modeling, and
More informationChemical Kinetics of HC Combustion
Spark Ignition Engine Combustion MAK65E Chemical Kinetics of HC Combustion Prof.Dr. Cem Soruşbay Istanbul Technical University Chemical Kinetics of HC Combustion Introduction Elementary reactions Multi-step
More informationDetonations in Hydrocarbon Fuel Blends
Detonations in Hydrocarbon Fuel Blends J.M. Austin and J.E. Shepherd Graduate Aeronautical Laboratories, California Institute of Technology Pasadena, California 91125 Explosion Dynamics Laboratory Report
More informationTheoretical Analysis on Deflagration-to-Detonation Transition *
heoretical Analysis on Deflagration-to-Detonation ransition * Yun-Feng Liu( 刘云峰 ),**, Huan Shen( 沈欢 ),, De-Liang Zhang( 张德良 ),, Zong-Lin Jiang( 姜宗林 ), Institute of echanics, Chinese Academy of Sciences,
More informationModelling of gas explosions
Modelling of gas explosions Knut Vågsæther Thesis submitted for the degree of Philosophiae Doctor. Porsgrunn, October 2010. Faculty of Technology Telemark University College Norway Faculty of Engineering
More informationDetonation Cell Width Measurements for H 2 N 2 O N 2 O 2 CH 4 NH 3 Mixtures
Detonation Cell Width Measurements for H 2 N 2 O N 2 O 2 CH 4 NH 3 Mixtures U. Pfahl, E. Schultz and J. E. Shepherd Graduate Aeronautical Laboratories California Institute of Technology Pasadena, CA 925
More informationDETONATION DIFFRACTION THROUGH AN ABRUPT AREA EXPANSION. Thesis by. Eric Schultz. In Partial Fulfillment of the Requirements.
DETONATION DIFFRACTION THROUGH AN ABRUPT AREA EXPANSION Thesis by Eric Schultz In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy California Institute of Technology Pasadena,
More informationTriple point shear-layers in gaseous detonation waves
4nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 9 - July 6, Sacramento, California AIAA 6-575 Triple point shear-layers in gaseous detonation waves L. Massa, J.M. Austin, T.L. Jackson, University
More informationPremixed, Nonpremixed and Partially Premixed Flames
Premixed, Nonpremixed and Partially Premixed Flames Flame (Reaction Zone) Flame (Reaction Zone) Flame (Reaction Zone) Fuel Air Fuel + Air φ 1 Products Fuel + Air φ > 1 F + A Air (+ F?) NONPREMIXED PREMIXED
More informationRegents Review Sheet 4 Naming Chemical Compounds, Shapes of Compounds and Balancing Chemical Equations
Regents Review Sheet 4 Naming Chemical Compounds, Shapes of Compounds and Balancing Chemical Equations These are some important points to remember about Naming Compounds. Use this sheet when you do the
More informationROLE OF CHEMICAL KINETICS ON THE DETONATION PROPERTIES OF HYDROGEN / NATURAL GAS / AIR MIXTURES
ROLE OF CHEMICAL KINETICS ON THE DETONATION PROPERTIES OF HYDROGEN / NATURAL GAS / AIR MIXTURES Chaumeix 1 N., Pichon 1 S., Lafosse 1 F., Udari 1 N., Paillard 1,2 C.-E. 1 Laboratoire de Combustion et Systèmes
More informationApplication of a Laser Induced Fluorescence Model to the Numerical Simulation of Detonation Waves in Hydrogen-Oxygen-Diluent Mixtures
Supplemental material for paper published in the International J of Hydrogen Energy, Vol. 30, 6044-6060, 2014. http://dx.doi.org/10.1016/j.ijhydene.2014.01.182 Application of a Laser Induced Fluorescence
More informationMeasurement and chemical kinetic model predictions of detonation cell size in methanol-oxygen mixtures
Shock Waves manuscript No. (will be inserted by the editor) Rachel Eaton Bo Zhang Jeffrey M. Bergthorson Hoi Dick Ng Measurement and chemical kinetic model predictions of detonation cell size in methanol-oxygen
More informationCHEMICAL KINETICS. Collision theory and concepts, activation energy and its importance VERY SHORT ANSWER QUESTIONS
Topic-3 CHEMICAL KINETICS Collision theory and concepts, activation energy and its importance 1. What is law of mass action? VERY SHORT ANSWER QUESTIONS This law relates rate of reaction with active mass
More informationUnidirectional Propagation of Gas Detonations in Channels with Sawtooth Walls
Naval Research Laboratory Washington, DC 20375-5320 NRL/MR/6404--10-9255 Unidirectional Propagation of Gas Detonations in Channels with Sawtooth Walls Vadim N. Gamezo Elaine S. Oran Center for Reactive
More informationMauro Valorani Dipartimento di Meccanica e Aeronautica, University of Rome
Classification of ignition regimes in thermally stratified n-heptane-air air mixtures using computational singular perturbation Saurabh Gupta, Hong G. Im Department of Mechanical Engineering, University
More informationTheory and Detonation Products Equations of State for a New Generation of Combined Effects Explosives. Dr. Ernest L. Baker
Theory and Detonation Products Equations of State for a New Generation of Combined Effects Explosives Dr. Ernest L. Baker W. Balas, L.I. Stiel, C. Capellos and J. Pincay 16 OCT 2007 Outline Combined Effects
More informationarxiv: v1 [physics.flu-dyn] 9 Aug 2017
arxiv:1708.02682v1 [physics.flu-dyn] 9 Aug 2017 Investigation of Turbulent Mixing and Local Reaction Rates on Deflagration to Detonation Transition in Methane-Oxygen Brian Maxwell a,c,, Andrzej Pekalski
More informationNumerical Investigation of Ignition Delay in Methane-Air Mixtures using Conditional Moment Closure
21 st ICDERS July 23-27, 27 Poitiers, France Numerical Investigation of Ignition Delay in Methane-Air Mixtures using Conditional Moment Closure Ahmad S. El Sayed, Cécile B. Devaud Department of Mechanical
More informationNumerical simulation of a rotating detonation with a realistic injector designed for separate supply of gaseous hydrogen and oxygen
Numerical simulation of a rotating detonation with a realistic injector designed for separate supply of gaseous hydrogen and oxygen Thomas Gaillard, Dmitry Davidenko, Francis Dupoirieux To cite this version:
More informationThe Direct Simulation of Detonations
Patrick D. O.Connor, Lyle N. Long, and James B. Anderson, "The Direct Simulation of Detonations," Invited Paper, AIAA Paper No. 2006-4411, AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Sacramento, CA,
More informationEnergy conversion in transient molecular plasmas:
Plenary lecture, 13 th International Conference on Flow Dynamics October 10-12, 2016, Sendai, Japan Energy conversion in transient molecular plasmas: Implications for plasma flow control and plasma assisted
More information05/04/2011 Tarik Al-Shemmeri 2
05/04/2011 Tarik Al-Shemmeri 1 05/04/2011 Tarik Al-Shemmeri 2 05/04/2011 Tarik Al-Shemmeri 3 05/04/2011 Tarik Al-Shemmeri 4 05/04/2011 Tarik Al-Shemmeri 5 05/04/2011 Tarik Al-Shemmeri 6 05/04/2011 Tarik
More informationIntroduction to Fluid Mechanics. Chapter 13 Compressible Flow. Fox, Pritchard, & McDonald
Introduction to Fluid Mechanics Chapter 13 Compressible Flow Main Topics Basic Equations for One-Dimensional Compressible Flow Isentropic Flow of an Ideal Gas Area Variation Flow in a Constant Area Duct
More informationHierarchical approach
Chemical mechanisms Examine (i) ways in which mechanisms are constructed, (ii)their dependence on rate and thermodynamic data and (iii) their evaluation using experimental targets Copyright 2011 by Michael
More informationSMART CART CONSERVATION OF MOMENTUM
NAME PERIOD DATE SMART CART CONSERVATION OF MOMENTUM Driving Question Objective How is the momentum and kinetic energy of a two-object system affected by a collision? Experimentally demonstrate that linear
More informationShock Reflection-Diffraction, Nonlinear Conservation Laws of Mixed Type, and von Neumann s Conjectures 1
Contents Preface xi I Shock Reflection-Diffraction, Nonlinear Conservation Laws of Mixed Type, and von Neumann s Conjectures 1 1 Shock Reflection-Diffraction, Nonlinear Partial Differential Equations of
More informationCh 16. Chemical Equilibria. Law of Mass Action. Writing Equil Constant Expressions Homogeneous Equilibria. 2NO 2 (g) N 2 O 4 (g)
Copyright 001 by Harcourt, Inc. All rights reserved.! Ch 16. Chemical Equilibria N O 4 (g) NO (g) The concept of equilibrium and K Writing equilibrium constant expressions Relationship between kinetics
More informationSELF-SIMILAR FLOW OF A MIXTURE OF A NON-IDEAL GAS AND SMALL SOLID PARTICLES WITH INCREASING ENERGY BEHIND A SHOCK WAVE UNDER A GRAVITATIONAL FIELD
SELF-SIMILAR FLOW OF A MIXTURE OF A NON-IDEAL GAS AND SMALL SOLID PARTICLES WITH INCREASING ENERGY BEHIND A SHOCK WAVE UNDER A GRAVITATIONAL FIELD Vishwakarma J.P. and Prerana Pathak 1 Deartment of Mathematics
More informationCh 16. Chemical Equilibria. Law of Mass Action. Writing Equil Constant Expressions Homogeneous Equilibria. 2NO 2 (g) N 2 O 4 (g) equilibrium
Copyright 001 by Harcourt, Inc. All rights reserved.! Ch 16. Chemical Equilibria N O 4 (g) NO (g) The concept of equilibrium and K Writing equilibrium constant expressions Relationship between kinetics
More information7/19/2011. Models of Solution. State of Equilibrium. State of Equilibrium Chemical Reaction
Models of Solution Chemistry- I State of Equilibrium A covered cup of coffee will not be colder than or warmer than the room temperature Heat is defined as a form of energy that flows from a high temperature
More informationOblique Detonation Wave Engine: Preliminary Design and Performance Prediction
Oblique Detonation Wave Engine: Preliminary Design and Performance Prediction A project present to The Faculty of the Department of Aerospace Engineering San Jose State University in partial fulfillment
More informationDetonation Characteristics Of Dimethyl Ether, Methanol and Ethanol Air Mixtures
24 th ICDERS July 28 - August 2, 213 Taipei, Taiwan Detonation Characteristics Of Dimethyl Ether, Methanol and Ethanol Air Mixtures Peter Diakow and Gaby Ciccarelli Queen's University Kingston, Ontario,
More informationCatalysis Lectures W.H. Green 5.68J/10.652J Spring Handouts: Norskov et al., J. Catalysis Imbihl and Ertl, Chem. Rev. (partial) Homework
Catalysis Lectures W.H. Green 5.68J/10.652J Spring 2003 Handouts: Norskov et al., J. Catalysis Imbihl and Ertl, Chem. Rev. (partial) Homework Major points: 1) Why reactions have barriers, and how catalysts
More informationarxiv: v1 [physics.flu-dyn] 7 Dec 2015
Chapman-Jouguet deflagrations and their transition to detonation Mohamed Saif a, Wentian Wang a, Andrzej Pekalski b, Marc Levin c, Matei I. Radulescu a a Department of Mechanical Engineering, University
More informationDirect Observations of Reaction Zone Structure in Propagating Detonations
Direct Observations of Reaction Zone Structure in Propagating Detonations F. Pintgen, C.A. Eckett 1, J.M. Austin, J.E. Shepherd Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena,
More informationWhat Are Type Ia Supernovae?
What Are Type Ia Supernovae? Max-Planck-Institut für Astrophysik Based on collaborations with: W. Hillebrandt (MPA Garching) S.E. Woosley (UC Santa Cruz) M. Reinecke (MPA Garching) B. Leibundgut (ESO Garching)
More informationCOMBUSTION OF THE BUTANOL ISOMERS: REACTION PATHWAYS AT ELEVATED PRESSURES FROM LOW-TO-HIGH TEMPERATURES
COMBUSTION OF THE BUTANOL ISOMERS: REACTION PATHWAYS AT ELEVATED PRESSURES FROM LOW-TO-HIGH TEMPERATURES Michael R. Harper, William H. Green* Massachusetts Institute of Technology, Department of Chemical
More informationSession 12 : Monopropellant Thrusters
Session 12 : Monoroellant Thrusters Electrothermal augmentation of chemical rockets was the first form of electric roulsion alied in sace vehicles. In its original imlementation, resistojets were used
More informationRayleigh-Taylor Unstable Flames
Rayleigh-Taylor Unstable Flames Elizabeth P. Hicks 1,2 and Robert Rosner 2 CIERA, Northwestern University 1 University of Chicago 2 CIERA Conference: September 2, 2011 1 Type Ia Supernovae Image: NASA
More informationSolutions to Chem 203 TT1 Booklet
Solutions to Chem 03 TT1 Booklet Chem03 TT1 Booklet Solutions to Gases Practice Problems Problem 1. Answer: C Increasing the temperature increases the kinetic energy of the molecules in the liquid causing
More informationL = 6.02 x mol Determine the number of particles and the amount of substance (in moles)
1.1 The Mole 1.1.1 - Apply the mole concept to substances A mole is the name given to a certain quantity. It represents 6.02 x 10 23 particles. This number is also known as Avogadro's constant, symbolised
More informationQuestions 1-3 relate to the following reaction: 1. The rate law for decomposition of N2O5(g) in the reaction above. B. is rate = k[n2o5] 2
Questions 1-3 relate to the following reaction: 2N2O5(g) 4NO2(g) + O2(g) 1. The rate law for decomposition of N2O5(g) in the reaction above A. is rate = k[n2o5] B. is rate = k[n2o5] 2 C. is rate = [NO2]
More informationAnalysis for Steady Propagation of a Generic Ram Accelerator/ Oblique Detonation Wave Engine Configuration
Analysis for Steady Propagation of a Generic Ram Accelerator/ Oblique Detonation Wave Engine Configuration J.M. Powers1, D.R. Fulton2, K.A. Gonthier3, and M.J. Grismer4 Department of Aerospace and Mechanical
More informationNumerical and Analytical Studies of the Dynamics of Gaseous Detonations
Numerical and Analytical Studies of the Dynamics of Gaseous Detonations Thesis by Christopher A. Eckett In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy I A I N S T I T
More information