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4 9 7 5 6 8 4. 4/ 1 5 2 0. 1 OI: D k o o B 0 | 0 0 0 0. 0 0 0 4. 9 7 5 6 8 0 0 6 1 8 7 9 5. 4/ 1 5 2 0. 1 OI: D g | or a. a ai c. ar p:// htt 3 | 1 0 2 6, 1 e n u n J o A R O O D N U B V NI U T MI R y b d e d a o nl w o D DYNAMICS OF REACTIVE SYSTEMS PART I: FLAMES AND CONFIGURATIONS 4 9 7 5 6 8 4. 14/ Edited by 5 2 0. J. R. Bowen 1 OI: University of Washington D k Seattle, Washington o o B 00 | J.-C. Leyer 0 0 0. Universite de Poitiers 0 0 0 Poitiers, France 4. 9 7 5 6 08 R. I. Soloukhin 0 16 Institute of Heat and Mass Transfer 8 7 9 BSSR Academy of Sciences 5. 14/ Minsk, USSR 5 2 0. 1 OI: D Volume 105 g | or PROGRESS IN a. a c.ai ASTRONAUTICS AND AERONAUTICS ar p:// htt 13 | Martin Summerfield, Series Editor-in-Chief 0 2 6, Princeton Combustion Research Laboratories, Inc. 1 ne Monmouth Junction, New Jersey u n J o A R O O Technical papers presented from the Tenth International Colloquium on D N Dynamics of Explosions and Reactive Systems, Berkeley, California, August U B V 1985, and subsequently revised for this volume. NI U T MI R Published by the American Institute of Aeronautics and Astronautics, Inc. y d b 1633 Broadway, New York, NY 10019 e d a o nl w o D 4 9 7 5 6 8 4. 4/ 1 5 2 0. 1 OI: D k o o 0 | B American Institute of Aeronautics and Astronautics, Inc. 0 New York, New York 0 0 0. 0 0 4.0 Library of Congress Cataloging in Publication Data 9 7 5 6 08 International Colloquium on Dynamics of Explosions and 0 16 Reactive Systems (10th: 1985:Berkeley, Calif.) 8 97 Dynamics of Reactive Systems. Part I. 5. 4/ Flames and Configurations. 1 5 2 (Progress in astronautics and aeronautics; v.105: Part I) 0. OI: 1 ''Technical papers presented from the Tenth D International Colloquium on Dynamics of Explosions and g | Reactive Systems, Berkeley, California, August 1985." or a. Companion volume to: Dynamics of explosions. a c.ai Includes index. p://ar 1. Flames—Congresses. 2. Configurations—Congresses. htt I. Bowen, J.R. (J. Raymond) II. Leyer, J.-C. III. Soloukhin, Rem 3 | Ivanovich. IV. Title. V. Series. 1 0 2 ISBN 0-930403-14-2 6, 1 e n u n J Copyright © 1986 by the American Institute of Aeronautics and o A Astronautics, Inc. All rights reserved. Reproduction or translation of any R OO part of this work beyond that permitted by Sections 107 and 108 of the U.S. D N Copyright Law without the permission of the copyright owner is unlawful. U B The code following this statement indicates the copyright owner's consent V NI that copies of articles in this volume may be made for personal or internal U use, on condition that the copier pay the per-copy fee ($2.00) plus the per- T MI page fee ($0.50) through the Copyright Clearance Center, Inc., 21 Congress R y Street, Salem, Mass. 01970. This consent does not extend to other kinds of b d copying, for which permission requests should be addressed to the publisher. e d oa Users should employ the following code when reporting copying from this nl w volume to the Copyright Clearance Center: o D 0-930403-14-2/86 $2.00+.50 4 9 7 5 6 8 4. 4/ 1 5 2 0. 1 OI: Progress in Astronautics and Aeronautics D k oo Series Editor-in-Chief B 0 | Martin Summerfield 0 0 0.0 Princeton Combustion Research Laboratories, Inc. 0 0 0 4. 9 7 5 6 8 00 Series Associate Editors 6 1 8 7 9 4/5. Burton I. Edelson Alien E. Fuhs 1 25 National A eronautics Naval Postgraduate School 0. 1 OI: and Space A dministration D org | Jack L. Kerrebrock a. aia Massachusetts Institute of Technology c. ar p:// 3 | htt Assistant Series Editor 1 0 2 6, Ruth F. Bryans 1 ne Ocala, Florida u n J o A R O O D N Norma J. Brennan Jeanne Godette U B V Director, Editorial Department Series Managing Editor NI U AIAA AIAA T MI R y b d e d a o nl w o D 4 9 7 5 6 8 4. 4/ 1 5 2 0. 1 OI: This page intentionally left blank D k o o B 0 | 0 0 0 0. 0 0 0 4. 9 7 5 6 8 0 0 6 1 8 7 9 5. 4/ 1 5 2 0. 1 OI: D g | or a. a ai c. ar p:// htt 3 | 1 0 2 6, 1 e n u n J o A R O O D N U B V NI U T MI R y b d e d a o nl w o D Table of Contents 4 9 7 65 Preface............................................................................xv 8 4. 4/ 1 5 2 Flame Structure in the Zero Mach Number Limit 0. 1 OI: and the Random Vortex Method............................................ 1 D k o Bo The Beauty of Combustion Fields and Their Aero-Thermo- 00 | Dynamic Significance..............................................................3 0 0.0 A.K. Oppenheim, University of California, Berkeley, California 0 0 0 4. 79 Vortex Methods for the Study of Turbulent Combustion 5 86 at a Low Mach Number..........................................................l4 0 0 16 A.J. Chorin, University of California, Berkeley, California 8 7 9 5. 4/ Chapter I Flame Ignition and Propagation...............................23 1 5 2 0. 1 OI: Numerical Analysis of Ignition of Hydrogen Spurted Into Air............25 D g | F. Takayama, Electrotechnical Laboratory, Tsukuba, Japan, S. Taki, a.or Fukui University, Fukui, Japan, T. Fujiwara, and A.K. Hayashi, Nagoya a c.ai University, Nagoya, Japan, and A. Sakurai, Toyko Denki University, p://ar Tokyo, Japan htt 3 | Flame Jet Ignition of Lean Fuel-Air Mixtures.................................38 1 0 6, 2 D.N. Rao Mittinti and E.K. Dabora, University of Connecticut, e 1 Storrs, Connecticut n u n J A o Inhibitory Action of Preflame Reactions on Flame Propagation R O in End Gas..........................................................................69 O D Y. Ohta, Nagoya Institute of Technology, Nagoya, Japan, and N U H. Takahashi, Meijo University, Nagoya, Japan B V NI U Ignition Modeling with Grid Adaption..........................................78 T MI A.E. Lutz, R.J. Kee, and H.A. Dwyer, Sandia National Laboratories, R y Liver more, California b d e d oa Consequence of Temperature-Pressure-Time History nl ow for Autoignition...................................................................93 D Y. Ohta, Nagoya Institute of Technology, Nagoya, Japan, A.K. Hayashi and T. Fujiwara, Nagoya University, Nagoya, Japan, and H. Takahashi, Meijo University, Nagoya, Japan Pulsed X-Ray and Optical Investigators of Unsteady High Velocity Jets Propagating in Gases......................................................104 V.K. Baev, A.N. Bazhaikin, A.A. Buzukov, B.P. Timoshenko, E.I. Bichenkov, and R.L. Rabinovich, USSR Academy of Sciences, Novosibirsk, USSR 4 79 Chapter II Diffusion and Premixed Flames ............;...............113 5 6 8 4. 4/ 1 5 Interaction of a Laminar Flame with Its Self-Generated 2 0. 1 Flow during Constant Volume Combustion...............................115 DOI: D. Dunn-Rankin and R.F. Sawyer, University of California, ok Berkeley, California o B 0 | 00 Cellular Flame Structures on a Cooled Porous Burner..................... 131 0 00. J.P. Vantelon, P.J. Pagni, and C.M. Dunsky, University of California, 0 4.0 Berkeley, California 9 7 5 6 08 Effects on Equilibrium Dissociation on the Structure and Extinction 0 6 1 of Laminar Diffusion Flames.................................................152 8 7 5.9 F.A. Williams, Princeton University, Princeton, New Jersey, 14/ and N. Peters, Rheinisch-Westfalische Technische Hochschule, 5 0.2 Aachen, West Germany 1 OI: g | D Effect of Curvature and Dilution on Unsteady, Premixed, or Laminar Flame Propagation..................................................167 a. aia K. Kailasanath and E.S. Oran, Naval Research Laboratory, c. ar Washington, D.C. p:// htt 3 | Simple Models of Constant Flames in Three Partially 1 20 Confined Geometries...........................................................l80 6, 1 P.H. Taylor, Shell Research Ltd., Chester, United Kingdom e n u n J o Two Adjacent, Coupled Laminar Diffusion Flames A R with Cylindrical Symmetry....................................................l92 O O D M.Y. Bahadori, C.-P. Li, and S.S. Penner, University of California, N U San Diego, La Jolla, California B V NI U Chemical Reactions in a Transient Natural Convective T MI Boundary Layer..................................................................208 R y P.D. Gandhi, University of Notre Dame, Notre Dame, Indiana, b d and A.M. Kanury, Oregon State University, Corvallis, Oregon e d a o nl w Flame Propagation Through a Layer with Varying o D Equivalence Ratio...............................................................233 Y. Ohki, Ashikaga Institute of Technology, Ashikaga, Japan, and S. Tsuge, University of Tsukuba, Ibaraki, Japan VI One-Dimensional Flame with Extended Reaction Zone....................246 T. Takeno, and M. Murayama, University of Tokyo, Tokyo, Japan Simulation of Stoichiometric Acetylene/, Ethylene/, Ethane/, and Methane/Air Premixed Flames.............................263 S. Fukutani and H. Jinno, Kyoto University, Kyoto, Japan 4 9 7 5 Chapter III Flame Instabilities and Acoustic Interactions.........281 6 8 4. 4/ 1 25 A Correlation Between Flame Structures and Acoustic Instabilities....283 0. DOI: 1 N. CDNaRrSab,Cihhad,t eTn.a yP-oMinaslaobt,r yS, .MF. rCanacned,el, and E. Esposito, k o o B Stability Study of an Oblique Flame Front Model...........................296 0 | 0 P. Garcia-Ybarra, Universidad Nacional de Educacion a Distancia, 0 0 0. Madrid, Spain, and R. Borghi, University de Rouen, 0 0 0 Mont-Saint Aignan, France 4. 9 7 5 86 The Evolution of the Transverse Gas Velocity Spectrum 0 60 Ahead of a Weakly Turbulent Hydrogen Flame..........................320 1 8 97 H. Nguyen Thi, G. Searby, and L. Boyer, University de Provence, 5. 4/ Marseille, France 1 5 2 10. An Experimental Analysis of Noise Sources in a Dump Combustor....333 OI: T. Poinsot, K. Hosseini, C. Le Chatelier, S.M. Candel, and D g | E. Esposito, CNRS, Chdtenay-Malabry, France or a. a c.ai Chapter IV Practical Combustion Configurations.................. 347 ar http:// A Numerical Model of a Pulse Combustor...................................349 3 | H.A. Dwyer, T.T. Bramlette, J.O. Keller, and B.R. Sanders, 1 20 Sandia National Laboratories, Livermore, California 6, 1 ne Radiation and Size Scaling of Large Gas and Gas/Oil u n J Diffusion Flames................................................................365 o RA H. Hustad, and O.K. Sonju, Norwegian Institute of Technology, O O Trondheim, Norway D N BU Experimental and Theoretical Study of Thermal Radiation NIV from Freely Burning Kerosene Pool Fires..................................388 T U J.M. Souil, J.P. Vantelon, and P. Joulain, Universite de Poitiers, MI Poitiers, France, and W.L. Grosshandler, Washington State R y University, Pullman, Washington b d e ad Residence Time in Flow Combustor............................................402 o wnl A. Giovannini, Office National d'Etudes et de Recherches o D Aerospatiales, Toulouse, France Author Index for Volume 105: Part I.....................................417 List of Series Volumes........................................................418 VII Table of Contents for Volume 105: Part II 4 9 7 65 Preface............................................................................................................ \xv 8 4. 4/ 51 Chapter I Models, Simulations, and Experiments in Turbulent 2 0. Reacting Flows 1 1 OI: D k Sensitivity Analysis of Turbulent Variable Density Round o Bo Jet and Diffusion Flame Flows...........................................................................................3 0 | F. Raiszadek and H.A. Dwyer, Universiity of California, Davis, California 0 0 0 0. Numerical Simulation of a Confined Shear Layer.....................................................................l8 0 00 K.K. Ng and A.F. Ghoniem, Massachusetts Institute of Technology, 4. Cambridge, Massachusetts 9 7 5 6 8 The Vortical Structure of Premixed Flames Stabilized 0 60 by a Circular Cylinder....................................................................................................50 1 78 T. Hasegawa, S. Yamaguchi, and N. Ohiwa, Nagoya Institute 5.9 of Technology, Nagoya, Japan 4/ 1 5 2 Numerical Simulation of Unsteady Mixing Layers....................................................................66 0. OI: 1 E.SW. aOshrainng, tJo.nP, . DB.oCr.i,s , aanndd FK.F. .K Garilianssateniant,h B, eNrakvealel yR Reseesaeracrhc hL Aabssoorcaitaotreys,, D Springfield, Virginia g | or a. Velocity and Density Measurements in a Planar Two-Steam, a ai Turbulent Mixing Layer..................................................................................................83 c. ar I.G. Shephard, J.L. Ellzey, and J.W. Daily, University of California, p:// Berkeley, California htt 13 | Two Dimensional Imaging of C2 in Turbulent Nonpremixed 20 Jet Flames...................................................................................................................99 6, R.W. Dibble, M.B. Long, and A. Masri, Sandia National Laboratories, 1 e Livermore, California n u on J Numerical Simulation of Turbulence Development A at Propagating Flame Fronts..........................................................................................110 R O T. Tsuruda and T. Hirano, University of Tokyo, Tokyo, Japan O D N U The Effect of Large-Scale Fluctuations on Flame Radiation......................................................123 V B W.L. Grosshandler, Washington State University, Pullman, Washington, NI and P. Joulain, Universitd de Poitiers, Poitiers, France U MIT Chapter II Heterogeneous Combustion 153 R y b d The Lean Flammability Limits of Hybrid Mixtures.................................................................155 e ad M. Gaug, R. Knystautas, and J.H.S. Lee, McGill University, Montreal, o nl Canada, and L. Nelson, W.B. Benedick, and J. Shepherd, Sandia w o National Laboratories, Albuquerque, New Mexico D Flame Structure in Dust and Hybrid Mixtures Near the Lean Flammability Limit..........................................................................................169 R. Klemens and P. Wolanski, Technical University of Warsaw, Warsaw, Poland viii Turbulent Burning Velocity Measurements for Dust/Air Mixtures in a Constant Volume Spherical Bomb.................................................................. 184 F.I. Tezok, C.W. Kauffman, M. Sichel, and J.A. Nicholls, The University of Michigan, Ann Arbor, Michigan Flame Propagation Due to Layered Combustion Dusts............................................................196 S.R. Srinath, C.W. Kauffman, J.A. Nicholls, and M. Sichel, The University of Michigan, Ann Arbor, Michigan 4 9 7 5 Stability of a Droplet Vaporizing in a Hot Atmosphere............................................................217 6 4.8 F.J. Higuera and A. Linan, Universidad Politecnia de Madrid, 4/ Madrid, Spain, 1 5 2 10. Droplet Ignition in Mixted Convection.................................................................................239 OI: R.H. Rangel and A.C. Fernandez-Pello, University of California, D Berkeley, California k o o B A Numerical Technique for the Solution of a Vaporizing 0 | Fuel Droplet...............................................................................................................253 0 00 G. Patnaik, Carnegie-Mellon University, Pittsburgh, Pennsylvania, 00. W.A. Sirignano, University of California, Irvine, California, 00 and H.A. Dwyer, and B.R. Sander, Sandia National Laboratories, 94. Livermore, California 7 5 6 08 Interaction of Flame Spreading, Combustion, and Fracture 0 6 of Single-Perforated Stick Propellants Under 1 78 Dynamic Conditions....................................................................................................267 9 5. M.M Athavale, K.C. Hsieh, W.H. Hsieh, J.M. Char, and K.K. Kuo, 14/ Pennslyvania State University, University Park, Pennsylvania 5 2 0. 1 OI: Chapter III Combustion Modeling and Kinetics 291 D g | a.or Interactions Between a Laminar Flame and End Gas Autoignition..............................................293 aia W.J. Pitz and C.K. Westbrook, Lawrence Livermore National Laboratory, arc. Livermore, California http:// On the Role of the Radical Pool in Combustion.....................................................................304 3 | J.R. Creighton, Lawrence Livermore National Laboratory, Livermore, 01 California, and A.K. Oppenheim, University of California, 6, 2 Berkeley, California 1 e n on Ju A bNyu Lmoecraicl aHl eAant aAlydsdisi toifo nth..e. .I.g..n..i.t.i.o.n.. .o.f. ..P..ie..m...ix..e.d.. .G...a.s.e..s.........................................................321 RA P.S. Tromans, and R.M. Furzeland, Shell Research Ltd., Chester, O United Kingdom O D N U Thermal Ignition and Minimum Ignition Energy B V in Oxygen-Ozone Mixtures.............................................................................................335 NI B. Raffel, J. Warnatz, H. Wolff, and J. Wolfrum, Universitat Heidelberg, T U Heidelberg, West Germany, and R.J. Kee, Sandia National Laboratories, MI Livermore, California R y d b Chemical Effects on Reflected-Shock Region in Combustible Gas..............................................347 de Y. Takano, Tottori University, Tottori, Japan, and T. Akamatsu, a nlo Kyoto University, Kyoto, Japan w o D Systematic Development of Reduced Reaction Mechanisms for Dynamic Modeling..................................................................................................365 M. Frenklach, Pennsylvania, State University, University Park, Pennsylvania, K. Kailasanath, and E.S. Oran, Naval Research Laboratory, Washington, D.C. IX

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