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This second edition of the classic on the thermochemistry of combustion now features five new chapters and updated coverage of significant recent developments in the field. Addressing both experimental as well as theoretical aspects, the book covers the thermochemical and combustion characteristics of all important types of energetic materials, such as explosives, propellants, and the new class of pyrolants, as well as related phenomena. It presents the fundamental bases of the energetics of materials, deflagration and detonation, thermochemical process of decomposition and combustion,…mehr
This second edition of the classic on the thermochemistry of combustion now features five new chapters and updated coverage of significant recent developments in the field. Addressing both experimental as well as theoretical aspects, the book covers the thermochemical and combustion characteristics of all important types of energetic materials, such as explosives, propellants, and the new class of pyrolants, as well as related phenomena. It presents the fundamental bases of the energetics of materials, deflagration and detonation, thermochemical process of decomposition and combustion, plus combustion wave structures. The book also goes on to discuss the combustion mechanisms of various types of energetic materials, propellants, and explosives, based on the heat transfer process in the combustion waves. The burning rate models are also presented as an aid to understanding the rate-controlling steps of combustion processes, thus demonstrating the relationships of burning rate versus pressure and initial temperature. As a major topic new to this edition, new propulsion methods such as duct rockets, ramjets, pulse motors and thrusters are described in detail, while appendices on flow field dynamics and shock wave propagation have been added.
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Autorenporträt
Dr. Kubota received a Doctorate from Princeton University in 1973, majoring in "Solid Propellant Combustion" and "Rocket Propulsion including Ducted Rocket Engine". His current position is Senior Research Scientist of Propellant Combustion Laboratory, Asahi Kasei Chemicals. Previously, he was Director, Third Research Center, Technical Research and Development Institute (TRDI), Japan Defense Agency, which is responsible for aircraft and missiles.
Inhaltsangabe
From the contents: Thermodynamics for energy conversion Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces Thermochemistry of combustion Generation of Heat Adiabatic Flame Temperature Chemical Reaction Combustion wave propagation Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials Energetics of Propellants and explosives Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives Combustion of crystelline and polymeric materials
Combustion of Crystalline Materials Combustion of Polymeric Materials
Combustion of Double-base propellants NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants Combustion of composite Propellants AP Composite Propellants N itramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants Combution of explosives Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena Combustion in rocket motors Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix IndexTHERMODYNAMICS FOR ENERGY CONVERSION Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces THERMOCHEMISTRY OF COMBUSTION Generation of Heat Adiabatic Flame Temperature Chemical Reaction COMBUSTION WAVE PROPAGATION Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials ENERGETICS OF PROPELLANTS AND EXPLOSIVES Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives COMBUSTION OF CRYSTALLINE AND POLYMERIC MATERIALS Combustion of Crystalline Materials Combustion of Polymeric Materials COMBUSTION OF DOUBLE-BASE PROPELLANTS NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants COMBUSTION OF COMPOSITE PROPELLANTS AP Composite Propellants Nitramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants COMBUSTION OF EXPLOSIVES Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena COMBUSTION IN ROCKET MOTOR Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix Index
From the contents: Thermodynamics for energy conversion Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces Thermochemistry of combustion Generation of Heat Adiabatic Flame Temperature Chemical Reaction Combustion wave propagation Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials Energetics of Propellants and explosives Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives Combustion of crystelline and polymeric materials
Combustion of Crystalline Materials Combustion of Polymeric Materials
Combustion of Double-base propellants NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants Combustion of composite Propellants AP Composite Propellants N itramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants Combution of explosives Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena Combustion in rocket motors Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix IndexTHERMODYNAMICS FOR ENERGY CONVERSION Fundamentals Thermodynamics in Flow Field Formation of Propulsive Forces THERMOCHEMISTRY OF COMBUSTION Generation of Heat Adiabatic Flame Temperature Chemical Reaction COMBUSTION WAVE PROPAGATION Reaction for Combustion Combustion Wave of Premixed Gas Structure of Combustion Wave Reaction for Ignition Combustion Wave of Energetic Materials ENERGETICS OF PROPELLANTS AND EXPLOSIVES Evaluation of Chemical Energy Crystalline and Polymeric Materials Classification of Propellants and Explosives Formulation of Propellants Nitropolymer Propellants Composite Propellants Formulation of Explosives COMBUSTION OF CRYSTALLINE AND POLYMERIC MATERIALS Combustion of Crystalline Materials Combustion of Polymeric Materials COMBUSTION OF DOUBLE-BASE PROPELLANTS NC-NG Propellants NC-TMETN Propellants Nitro-Azide Propellants Catalyzed Double-Base Propellants COMBUSTION OF COMPOSITE PROPELLANTS AP Composite Propellants Nitramine Composite Propellants TAGN Composite Propellants Composite Modified Double-Base Propellants COMBUSTION OF EXPLOSIVES Detonation Velocity and Pressure Density and Detonation Velocity Applications of Detonation Phenomena COMBUSTION IN ROCKET MOTOR Combustion Phenomena in Rocket Motor Ignition Transient Erosive Burning Wired propellant Burning; combustion Instability Ducted Rocket Engine Nomenclature Appendix Index
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