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High power laser propulsion / / Yuri A. Rezunkov
| High power laser propulsion / / Yuri A. Rezunkov |
| Autore | Rezunkov Yuri A. |
| Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2021] |
| Descrizione fisica | 1 online resource (307 pages) |
| Disciplina | 629.134353 |
| Collana | Springer Series on Atomic, Optical, and Plasma Physics |
| Soggetto topico |
Propulsion systems
Lasers in astronautics |
| ISBN | 3-030-79693-0 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Preface -- Acknowledgments -- Contents -- About the Author -- Abbreviations -- Chapter 1: A Brief History of Laser Propulsion -- 1.1 Introduction -- 1.2 Main Stages of Laser-Propulsion Developments -- 1.3 Physical Processes Underlying Laser Propulsion -- 1.3.1 General Classification of the Laser-Propulsion Phenomena -- 1.3.2 Basic Thrust Characteristics of Laser-Propulsion Engines -- 1.4 General Concepts of Laser Propulsion -- 1.4.1 Launching Space Vehicles into Low Earth Orbits with Laser Propulsion -- 1.4.2 Laser Propulsion for the Correction of LEO Satellites -- 1.4.3 Interorbital Missions of Space Vehicles with the Laser Propulsion -- 1.5 Original Concepts of High-Power Laser Propulsion -- 1.5.1 The ``4P´´ Vehicles -- 1.5.2 Lightcraft Technology Demonstrator (LTD) -- 1.5.3 Laser Impulse Space Propulsion-LISP -- 1.5.4 Principal Concept Design of the High-power Laser-Propulsion Systems -- References -- Chapter 2: Basic Gas-Dynamic Theories of the Laser Air-Breathing and Rocket Propulsion -- 2.1 Introduction -- 2.2 Gas-dynamic Theory of Laser Propulsion -- 2.2.1 Specific Properties of Pulsejet Laser Propulsion -- 2.2.2 Rocket Laser Propulsion at Space Conditions -- 2.2.2.1 Choice of a Propellant for Space Laser Propulsion -- 2.2.2.2 Determination of the Jet Nozzle Designs -- 2.3 Physics of Laser Plasma Ignited in Gases as Applied to Laser Propulsion -- 2.3.1 Model of Multi-Ionized Plasma Ignited by Laser Pulses in Gases -- 2.3.2 Conversion Efficiency of Laser Power into Plasma Temperature -- 2.4 Numerical Calculations of Non-stationary and Non-isentropic Gas Flows as Applied to Laser Propulsion -- 2.4.1 Perfect Gas Flow Models and Numerical Algorithms to Calculate Gas Flow of Pulsejet Laser Propulsion -- 2.4.2 Model of Equilibrium (Thermal) Plasma -- 2.4.3 Model of Non-equilibrium Plasma as Applied to Pulsejet Laser Propulsion.
2.4.4 Discussion on the Applicability of Various Models of Plasma Ignited -- References -- Chapter 3: Laser Ablation of Solid Materials, Laser Ablation Propulsion -- 3.1 Introduction -- 3.2 Physical Phenomena Underlying of Laser Ablation Propulsion -- 3.2.1 Basic Concept of Developed Evaporation of High-Melting and Low-Melting Materials -- 3.2.2 Simplified Gas-Dynamics Model of Laser ablation Propulsion -- 3.2.3 ``Absorption Explosion´´ Model of Plasma Ignition at Laser Ablation of Solid Targets -- 3.2.4 Gas-Dynamic Models of the Laser Radiation Interaction with Ionized Gas (Gaseous Plasma) -- 3.3 Effects of Solid Target Structure on Laser Ablation Propulsion -- 3.3.1 Direct Laser Ablation Propulsion -- 3.3.2 Combined Laser Ablation Propulsion -- 3.3.3 Confined Laser Ablation of Multilayer Structured Targets -- 3.4 Laser Ablation Propulsion Based on Ablation of High-Energy Polymers -- 3.4.1 Basic Plasma-chemical Reactions Proceeding in the CHO-Polymer Vapor Under Laser Radiation -- 3.4.2 Similarity Laws of Laser Ablation Propulsion Based on Polymer Propellants -- 3.5 Semi-empirical Models of Laser ablation Propulsion Based on CHO-Polymers -- 3.5.1 Gas-Dynamics of the Laser Ablation Propulsion -- 3.5.2 Vapor and Plasma Models of the Laser ablation Propulsion Using Critical Laser Power Flux -- 3.6 Efficiency of the Laser Ablation Propulsion Based on CHO-Polymers -- References -- Chapter 4: Aerospace Laser-Propulsion Engine -- 4.1 Introduction -- 4.2 The Aerospace Laser-Propulsion Engine Conception -- 4.2.1 Designing of Two-Mirror Beam Concentrator -- 4.2.2 Optical Model of the Two-Mirror Beam Concentrator -- 4.2.3 Numerical Techniques to Develop the Two-Mirror Beam Concentrator -- 4.3 ASLPE Thrust Characteristics in a Pulsed Mode of Operation -- 4.4 Adaptation of ASLPE for Continuous Wave (CW) Laser Propulsion -- 4.4.1 Principles of CW Laser Propulsion. 4.4.2 CW ASLPE Thrust Characteristics -- 4.5 Analysis of Available Technologies as Applied to ASLPE Development and its Engineering Constraints -- 4.5.1 Effects of Slit on Thrust Production -- 4.5.2 Thermo-physical Model of the ASLPE Device -- 4.6 Preliminary Conclusion -- References -- Chapter 5: Supersonic Laser Propulsion -- 5.1 Introduction -- 5.2 Lightcraft Engineering Version Adapted to the Pulsejet Supersonic Laser Propulsion -- 5.2.1 Perspective Designs of the Lightcraft -- 5.2.2 Intermediate Conclusion -- 5.3 Physical Phenomena Going with Ramjet Supersonic Laser Propulsion -- 5.3.1 Gas-Dynamics Effects Induced by Lasers in a Supersonic Gas Flow -- 5.4 Merging of Individual Shock Waves into a Quasi-Stationary Integrated Shock Wave -- 5.5 Supersonic Laser Ablation Propulsion -- 5.5.1 The Effects of Gas Jet Injection into Supersonic Gas Flows -- 5.5.2 Theoretical Model of Supersonic Laser Ablation Propulsion -- 5.5.3 Thrust Characteristics of Supersonic Laser Ablation Propulsion -- 5.5.4 Peculiar Properties of Thrust Production at the Supersonic Laser Ablation Propulsion -- 5.6 Conclusion -- References -- Chapter 6: Space Mini-vehicles with Laser Propulsion -- 6.1 Introduction to the Problem -- 6.2 Scenario of the SMV Orbital Maneuvers -- 6.3 Space Debris Removal Out of Geosynchronous Earth Orbit (GEO) by Using Laser-Propelled Space Mini-vehicles -- 6.4 Onboard Laser-Propulsion System as Applied to SMV -- 6.4.1 Receiver Telescope -- 6.4.2 Optical Turret -- 6.4.3 Optical Switch -- 6.4.4 The Unit of Laser-Propulsion Engines -- 6.4.5 Requirements to Optical Elements of the Onboard Laser-Propulsion System -- 6.5 Brief Outcome -- References -- Chapter 7: Laser Power Transfer to Space Vehicles with Laser Propulsion -- 7.1 Introduction into the Problem. 7.2 Models of the Aerosols and Gases Attenuation, Absorption, and Scattering of Laser Radiation in the Upper Atmosphere -- 7.2.1 Models of the Atmospheric Aerosols and Gases -- 7.2.2 Nonlinear Effects Developed During Propagation of High-Power Laser Radiation in the Upper Atmosphere -- 7.3 Self-Empirical Models of the Upper Atmosphere Turbulence -- 7.4 Phase and Intensity Profiles of the Laser Beam That Passed Through a Turbulent Atmosphere -- 7.4.1 Tentative Conclusion -- 7.5 Basic Atmospheric Effects Limiting Delivery of the Airborne Laser Power to Space Vehicle -- 7.5.1 Scenario of Laser Power Delivery to a Space Vehicle -- 7.5.2 Turbulence Effects on a Laser Beam as Applied to High-Power Laser Propulsion -- 7.6 Adaptive Laser Systems for the High-Power Laser Propulsion -- 7.6.1 Statement of the Problem -- 7.6.2 Adaptive Optical Laser Circuits and Special Equipment -- 7.6.2.1 Beam Wave Front Analyzers (BWA) -- 7.6.2.2 Beam Wave Front Phase Correctors -- 7.6.3 Laser Adaptive Optical Systems as Applied to Beaming a Remote Target -- 7.6.3.1 Linear Adaptive Laser Systems -- 7.6.3.2 Nonlinear Adaptive System Based on the Interaction of Laser Radiations with a Nonlinear Optical Medium -- 7.6.4 Principal Outcomes -- References -- Conclusion -- Index. |
| Record Nr. | UNINA-9910495191903321 |
Rezunkov Yuri A.
|
||
| Cham, Switzerland : , : Springer, , [2021] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
High power laser propulsion / / Yuri A. Rezunkov
| High power laser propulsion / / Yuri A. Rezunkov |
| Autore | Rezunkov Yuri A. |
| Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2021] |
| Descrizione fisica | 1 online resource (307 pages) |
| Disciplina | 629.134353 |
| Collana | Springer Series on Atomic, Optical, and Plasma Physics |
| Soggetto topico |
Propulsion systems
Lasers in astronautics |
| ISBN | 3-030-79693-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Preface -- Acknowledgments -- Contents -- About the Author -- Abbreviations -- Chapter 1: A Brief History of Laser Propulsion -- 1.1 Introduction -- 1.2 Main Stages of Laser-Propulsion Developments -- 1.3 Physical Processes Underlying Laser Propulsion -- 1.3.1 General Classification of the Laser-Propulsion Phenomena -- 1.3.2 Basic Thrust Characteristics of Laser-Propulsion Engines -- 1.4 General Concepts of Laser Propulsion -- 1.4.1 Launching Space Vehicles into Low Earth Orbits with Laser Propulsion -- 1.4.2 Laser Propulsion for the Correction of LEO Satellites -- 1.4.3 Interorbital Missions of Space Vehicles with the Laser Propulsion -- 1.5 Original Concepts of High-Power Laser Propulsion -- 1.5.1 The ``4P´´ Vehicles -- 1.5.2 Lightcraft Technology Demonstrator (LTD) -- 1.5.3 Laser Impulse Space Propulsion-LISP -- 1.5.4 Principal Concept Design of the High-power Laser-Propulsion Systems -- References -- Chapter 2: Basic Gas-Dynamic Theories of the Laser Air-Breathing and Rocket Propulsion -- 2.1 Introduction -- 2.2 Gas-dynamic Theory of Laser Propulsion -- 2.2.1 Specific Properties of Pulsejet Laser Propulsion -- 2.2.2 Rocket Laser Propulsion at Space Conditions -- 2.2.2.1 Choice of a Propellant for Space Laser Propulsion -- 2.2.2.2 Determination of the Jet Nozzle Designs -- 2.3 Physics of Laser Plasma Ignited in Gases as Applied to Laser Propulsion -- 2.3.1 Model of Multi-Ionized Plasma Ignited by Laser Pulses in Gases -- 2.3.2 Conversion Efficiency of Laser Power into Plasma Temperature -- 2.4 Numerical Calculations of Non-stationary and Non-isentropic Gas Flows as Applied to Laser Propulsion -- 2.4.1 Perfect Gas Flow Models and Numerical Algorithms to Calculate Gas Flow of Pulsejet Laser Propulsion -- 2.4.2 Model of Equilibrium (Thermal) Plasma -- 2.4.3 Model of Non-equilibrium Plasma as Applied to Pulsejet Laser Propulsion.
2.4.4 Discussion on the Applicability of Various Models of Plasma Ignited -- References -- Chapter 3: Laser Ablation of Solid Materials, Laser Ablation Propulsion -- 3.1 Introduction -- 3.2 Physical Phenomena Underlying of Laser Ablation Propulsion -- 3.2.1 Basic Concept of Developed Evaporation of High-Melting and Low-Melting Materials -- 3.2.2 Simplified Gas-Dynamics Model of Laser ablation Propulsion -- 3.2.3 ``Absorption Explosion´´ Model of Plasma Ignition at Laser Ablation of Solid Targets -- 3.2.4 Gas-Dynamic Models of the Laser Radiation Interaction with Ionized Gas (Gaseous Plasma) -- 3.3 Effects of Solid Target Structure on Laser Ablation Propulsion -- 3.3.1 Direct Laser Ablation Propulsion -- 3.3.2 Combined Laser Ablation Propulsion -- 3.3.3 Confined Laser Ablation of Multilayer Structured Targets -- 3.4 Laser Ablation Propulsion Based on Ablation of High-Energy Polymers -- 3.4.1 Basic Plasma-chemical Reactions Proceeding in the CHO-Polymer Vapor Under Laser Radiation -- 3.4.2 Similarity Laws of Laser Ablation Propulsion Based on Polymer Propellants -- 3.5 Semi-empirical Models of Laser ablation Propulsion Based on CHO-Polymers -- 3.5.1 Gas-Dynamics of the Laser Ablation Propulsion -- 3.5.2 Vapor and Plasma Models of the Laser ablation Propulsion Using Critical Laser Power Flux -- 3.6 Efficiency of the Laser Ablation Propulsion Based on CHO-Polymers -- References -- Chapter 4: Aerospace Laser-Propulsion Engine -- 4.1 Introduction -- 4.2 The Aerospace Laser-Propulsion Engine Conception -- 4.2.1 Designing of Two-Mirror Beam Concentrator -- 4.2.2 Optical Model of the Two-Mirror Beam Concentrator -- 4.2.3 Numerical Techniques to Develop the Two-Mirror Beam Concentrator -- 4.3 ASLPE Thrust Characteristics in a Pulsed Mode of Operation -- 4.4 Adaptation of ASLPE for Continuous Wave (CW) Laser Propulsion -- 4.4.1 Principles of CW Laser Propulsion. 4.4.2 CW ASLPE Thrust Characteristics -- 4.5 Analysis of Available Technologies as Applied to ASLPE Development and its Engineering Constraints -- 4.5.1 Effects of Slit on Thrust Production -- 4.5.2 Thermo-physical Model of the ASLPE Device -- 4.6 Preliminary Conclusion -- References -- Chapter 5: Supersonic Laser Propulsion -- 5.1 Introduction -- 5.2 Lightcraft Engineering Version Adapted to the Pulsejet Supersonic Laser Propulsion -- 5.2.1 Perspective Designs of the Lightcraft -- 5.2.2 Intermediate Conclusion -- 5.3 Physical Phenomena Going with Ramjet Supersonic Laser Propulsion -- 5.3.1 Gas-Dynamics Effects Induced by Lasers in a Supersonic Gas Flow -- 5.4 Merging of Individual Shock Waves into a Quasi-Stationary Integrated Shock Wave -- 5.5 Supersonic Laser Ablation Propulsion -- 5.5.1 The Effects of Gas Jet Injection into Supersonic Gas Flows -- 5.5.2 Theoretical Model of Supersonic Laser Ablation Propulsion -- 5.5.3 Thrust Characteristics of Supersonic Laser Ablation Propulsion -- 5.5.4 Peculiar Properties of Thrust Production at the Supersonic Laser Ablation Propulsion -- 5.6 Conclusion -- References -- Chapter 6: Space Mini-vehicles with Laser Propulsion -- 6.1 Introduction to the Problem -- 6.2 Scenario of the SMV Orbital Maneuvers -- 6.3 Space Debris Removal Out of Geosynchronous Earth Orbit (GEO) by Using Laser-Propelled Space Mini-vehicles -- 6.4 Onboard Laser-Propulsion System as Applied to SMV -- 6.4.1 Receiver Telescope -- 6.4.2 Optical Turret -- 6.4.3 Optical Switch -- 6.4.4 The Unit of Laser-Propulsion Engines -- 6.4.5 Requirements to Optical Elements of the Onboard Laser-Propulsion System -- 6.5 Brief Outcome -- References -- Chapter 7: Laser Power Transfer to Space Vehicles with Laser Propulsion -- 7.1 Introduction into the Problem. 7.2 Models of the Aerosols and Gases Attenuation, Absorption, and Scattering of Laser Radiation in the Upper Atmosphere -- 7.2.1 Models of the Atmospheric Aerosols and Gases -- 7.2.2 Nonlinear Effects Developed During Propagation of High-Power Laser Radiation in the Upper Atmosphere -- 7.3 Self-Empirical Models of the Upper Atmosphere Turbulence -- 7.4 Phase and Intensity Profiles of the Laser Beam That Passed Through a Turbulent Atmosphere -- 7.4.1 Tentative Conclusion -- 7.5 Basic Atmospheric Effects Limiting Delivery of the Airborne Laser Power to Space Vehicle -- 7.5.1 Scenario of Laser Power Delivery to a Space Vehicle -- 7.5.2 Turbulence Effects on a Laser Beam as Applied to High-Power Laser Propulsion -- 7.6 Adaptive Laser Systems for the High-Power Laser Propulsion -- 7.6.1 Statement of the Problem -- 7.6.2 Adaptive Optical Laser Circuits and Special Equipment -- 7.6.2.1 Beam Wave Front Analyzers (BWA) -- 7.6.2.2 Beam Wave Front Phase Correctors -- 7.6.3 Laser Adaptive Optical Systems as Applied to Beaming a Remote Target -- 7.6.3.1 Linear Adaptive Laser Systems -- 7.6.3.2 Nonlinear Adaptive System Based on the Interaction of Laser Radiations with a Nonlinear Optical Medium -- 7.6.4 Principal Outcomes -- References -- Conclusion -- Index. |
| Record Nr. | UNISA-996466739003316 |
|
Rezunkov Yuri A.
|
||
| Cham, Switzerland : , : Springer, , [2021] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
| ||
High-Pressure Flows for Propulsion Applications
| High-Pressure Flows for Propulsion Applications |
| Autore | Bellan Josette |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Reston : , : American Institute of Aeronautics & Astronautics, , 2020 |
| Descrizione fisica | 1 online resource (804 pages) |
| Disciplina | 629.475 |
| Collana | Progress in Astronautics and Aeronautics |
| Soggetto topico | Propulsion systems |
| ISBN |
1-5231-4088-7
1-62410-581-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Title page -- Copyright -- Table of Contents -- Preface -- 1 Microgravity Research on Quasi-Steady and Unsteady Combustion of Fuel Droplet at High Pressures -- I. INTRODUCTION -- II. FUEL DROPLET EVAPORATION -- III. FUEL DROPLET COMBUSTION -- IV. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 2 Laboratory Experiments of High-Pressure Fluid Drops -- I. INTRODUCTION -- II. INTRODUCTION TO THERMODYNAMICS OF INTERFACES -- III. EXPERIMENTAL TEST RIG: A HIGH-PRESSURE APPARATUS FOR FALLING DROPLETS -- IV. OPTICAL TECHNIQUES: PROGRESS ON DROPLET CHARACTERIZATION AT HIGH PRESSURE -- V. RESULTS -- VI. ON THE LIMITS OF VLE FORMULATIONS -- VII. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 3 Optical Diagnostics for Sprays at High Pressure -- I. INTRODUCTION -- II. OPTICAL MEASUREMENTS AT HIGH PRESSURE AND TEMPERATURE -- III. WHITE-LIGHT IMAGING -- IV. LASER IMAGING -- V. TECHNIQUES THAT COULD POTENTIALLY BROADEN THE SCOPE OF MEASUREMENTS -- VI. OVERVIEW -- REFERENCES -- 4 Supercritical Coaxial Jet Disintegration -- NOMENCLATURE -- SUBSCRIPTS -- I. INTRODUCTION -- II. EXPERIMENTAL FACILITY -- III. WORKING FLUID AND EXPERIMENTAL TECHNIQUE -- IV. RESULTS -- V. CONCLUSIONS -- REFERENCES -- 5 High-Pressure Experiments Relevant to Rocket Propulsion -- I. INTRODUCTION -- II. BACKGROUND AND PAST EXPERIMENTS IN MODEL ROCKET COMBUSTORS -- III. MEASUREMENT AND DATA ANALYSIS OVERVIEW -- IV. MODAL DECOMPOSITION METHODS -- V. QUANTITATIVE OPTICAL COMPARISONS -- VI. SUMMARY AND CONCLUSIONS -- REFERENCES -- 6 Forced and Unforced Shear Coaxial Mixing and Combustion at Subcritical and Supercritical Pressures -- I. INTRODUCTION -- II. BACKGROUND: COAXIAL JET -- III. EXPERIMENTAL FACILITIES AND INSTRUMENTATION -- IV. RESULTS -- V. CONCLUSIONS -- REFERENCES -- 7 Measurement of Heat Transfer in Liquid Rocket Combustors -- NOMENCLATURE -- SUBSCRIPTS -- SUPERSCRIPTS.
I. INTRODUCTION -- II. HEAT-TRANSFER MEASUREMENT METHODOLOGIES -- III. EXAMPLES OF HEAT-FLUX MEASUREMENTS -- IV. DISCUSSION OF HEAT-FLUX MEASUREMENT APPROACHES -- REFERENCES -- 8 Characterization of Droplet Nucleation Inside Supercritical Ethylene Jets Using Small-Angle X-Ray Scattering Technique -- I. INTRODUCTION -- II. EXPERIMENTAL METHODS -- III. SMALL-ANGLE X-RAY SCATTERING -- IV. DATA REDUCTION -- V. RESULTS AND DISCUSSION -- VI. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 9 Empirical Fundamental Equations of State for Pure Fluids and Mixtures -- I. INTRODUCTION -- II. EQUATIONS OF STATE -- III. FITTING EQUATIONS OF STATE -- IV. PERFORMANCE OF EQUATIONS OF STATE AND FUTURE CHALLENGES -- V. CONCLUSION -- REFERENCES -- 10 Molecular Simulations to Research Supercritical Fuel Properties -- I. INTRODUCTION -- II. MOLECULAR APPROACH FOR RESEARCHING SUPERCRITICAL FLUIDS -- III. MC SIMULATIONS OF THE PHASE EQUILIBRIUM DIAGRAMS OF -- ALKANE/NITROGEN MIXTURES USING VARIOUS POTENTIALS -- IV. MD SIMULATIONS OF AN -- HEPTANE DROPLET VAPORIZING INTO NITROGEN AT VARIOUS AMBIENT TEMPERATURES AND PRESSURES -- ACKNOWLEDGMENT -- REFERENCES -- 11 Large Eddy Simulations of High-Pressure Jets: Effect of Subgrid-Scale Modeling -- I. INTRODUCTION -- II. GOVERNING EQUATIONS AND NUMERICAL METHOD -- III. NUMERICAL ASPECTS -- IV. CONFIGURATION, BOUNDARY CONDITIONS AND INITIAL CONDITIONS -- V. RESULTS AND DISCUSSION -- VI. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 12 High Pressure Flames with Multicomponent Transport -- I. INTRODUCTION -- II. NONIDEAL FLUIDS -- III. BINARY MIXING LAYERS -- IV. FREELY PROPAGATING PREMIXED FLAMES -- V. STRAINED FLAMES -- VI. TRANSCRITICAL DIFFUSION FLAMES -- VII. CONCLUSION -- REFERENCES -- 13 Large-Eddy Simulation of Cryogenic Jet Injection at Supercritical Pressures -- I. INTRODUCTION -- II. THERMODYNAMICS MODEL. III. CRYOGENIC SINGLE-COMPONENT INJECTION AT SUPERCRITICAL PRESSURE -- IV. CRYOGENIC BINARY COMPONENT INJECTION AT SUPERCRITICAL PRESSURE -- V. CONCLUSION -- ACKNOWLEDGMENTS -- REFERENCES -- 14 Detailed Modeling of Supercritical Jets and Flames -- I. INTRODUCTION -- II. FLUID PROPERTIES IN SUPERCRITICAL ENVIRONMENTS -- III. KINETIC MODELS FOR HIGH-PRESSURE COMBUSTION -- IV. METHODOLOGY FOR ROBUST AND ACCURATE SIMULATIONS OF SUPERCRITICAL FLUIDS WITH LARGE DENSITY CONTRASTS -- V. ROBUST SOLVERS FOR STIFF CHEMISTRY -- VI. LES OF LOX/GH2 SHEAR-COAXIAL JET FLAME AT SUPERCRITICAL PRESSURE -- VII. CONCLUSIONS -- REFERENCES -- 15 Modeling and Simulations of High-Pressure Practical Flows -- I. INTRODUCTION -- II. NUMERICAL TOOLS FOR HIGH-PRESSURE REACTING FLOW SIMULATION -- III. COUPLING REAL-GAS TABULATED THERMOCHEMISTRY AND COMPRESSIBLE LES SOLVER -- IV. SIMULATION OF REACTING AND NONREACTING TURBULENT FLOWS -- V. CONCLUSION -- ACKNOWLEDGMENTS -- APPENDIX A. AEXPRESSION OF THE HEAT CAPACITY AT CONSTANT PRESSURE ( -- APPENDIX B. 2-D CONVECTION OF A MIXTURE FRACTION POCKET [MIXT] -- APPENDIX C. COUPLING THE REAL-GAS TABULATED THERMOCHEMISTRY WITH A LOW-MACH CODE -- REFERENCES -- 16 Large-Eddy Simulation of Liquid Injection and Combustion Processes in High-Pressure Systems -- I. INTRODUCTION -- II. GOVERNING EQUATIONS AND SUBMODEL FORMULATIONS -- III. RESULTS AND DISCUSSION -- IV. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- APPENDIX A. THERMODYNAMIC DERIVATIVES AS FUNCTION OF COMPRESSIBILITY FACTOR FOR THE CUBIC EQUATIONS OF STATE -- APPENDIX B. DEPARTURE FUNCTIONS FOR CUBIC EQUATIONS OF STATE -- REFERENCES -- 17 Simulation of the High-Pressure Combustion Process in Diesel Engines -- NOMENCLATURE -- SUPERSCRIPT -- SUBSCRIPT -- I. INTRODUCTION -- II. DIESEL SPRAY MODEL -- III. GOVERNING EQUATIONS FOR THE FLUID PHASE -- IV. COMBUSTION MODEL. V. CONSTANT-VOLUME COMBUSTION CHAMBER VALIDATIONS -- VI. DIESEL ENGINE SIMULATIONS -- VII. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- Index. |
| Record Nr. | UNINA-9910795671403321 |
|
Bellan Josette
|
||
| Reston : , : American Institute of Aeronautics & Astronautics, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
High-Pressure Flows for Propulsion Applications
| High-Pressure Flows for Propulsion Applications |
| Autore | Bellan Josette |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Reston : , : American Institute of Aeronautics & Astronautics, , 2020 |
| Descrizione fisica | 1 online resource (804 pages) |
| Disciplina | 629.475 |
| Collana | Progress in Astronautics and Aeronautics |
| Soggetto topico | Propulsion systems |
| ISBN |
1-5231-4088-7
1-62410-581-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Title page -- Copyright -- Table of Contents -- Preface -- 1 Microgravity Research on Quasi-Steady and Unsteady Combustion of Fuel Droplet at High Pressures -- I. INTRODUCTION -- II. FUEL DROPLET EVAPORATION -- III. FUEL DROPLET COMBUSTION -- IV. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 2 Laboratory Experiments of High-Pressure Fluid Drops -- I. INTRODUCTION -- II. INTRODUCTION TO THERMODYNAMICS OF INTERFACES -- III. EXPERIMENTAL TEST RIG: A HIGH-PRESSURE APPARATUS FOR FALLING DROPLETS -- IV. OPTICAL TECHNIQUES: PROGRESS ON DROPLET CHARACTERIZATION AT HIGH PRESSURE -- V. RESULTS -- VI. ON THE LIMITS OF VLE FORMULATIONS -- VII. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 3 Optical Diagnostics for Sprays at High Pressure -- I. INTRODUCTION -- II. OPTICAL MEASUREMENTS AT HIGH PRESSURE AND TEMPERATURE -- III. WHITE-LIGHT IMAGING -- IV. LASER IMAGING -- V. TECHNIQUES THAT COULD POTENTIALLY BROADEN THE SCOPE OF MEASUREMENTS -- VI. OVERVIEW -- REFERENCES -- 4 Supercritical Coaxial Jet Disintegration -- NOMENCLATURE -- SUBSCRIPTS -- I. INTRODUCTION -- II. EXPERIMENTAL FACILITY -- III. WORKING FLUID AND EXPERIMENTAL TECHNIQUE -- IV. RESULTS -- V. CONCLUSIONS -- REFERENCES -- 5 High-Pressure Experiments Relevant to Rocket Propulsion -- I. INTRODUCTION -- II. BACKGROUND AND PAST EXPERIMENTS IN MODEL ROCKET COMBUSTORS -- III. MEASUREMENT AND DATA ANALYSIS OVERVIEW -- IV. MODAL DECOMPOSITION METHODS -- V. QUANTITATIVE OPTICAL COMPARISONS -- VI. SUMMARY AND CONCLUSIONS -- REFERENCES -- 6 Forced and Unforced Shear Coaxial Mixing and Combustion at Subcritical and Supercritical Pressures -- I. INTRODUCTION -- II. BACKGROUND: COAXIAL JET -- III. EXPERIMENTAL FACILITIES AND INSTRUMENTATION -- IV. RESULTS -- V. CONCLUSIONS -- REFERENCES -- 7 Measurement of Heat Transfer in Liquid Rocket Combustors -- NOMENCLATURE -- SUBSCRIPTS -- SUPERSCRIPTS.
I. INTRODUCTION -- II. HEAT-TRANSFER MEASUREMENT METHODOLOGIES -- III. EXAMPLES OF HEAT-FLUX MEASUREMENTS -- IV. DISCUSSION OF HEAT-FLUX MEASUREMENT APPROACHES -- REFERENCES -- 8 Characterization of Droplet Nucleation Inside Supercritical Ethylene Jets Using Small-Angle X-Ray Scattering Technique -- I. INTRODUCTION -- II. EXPERIMENTAL METHODS -- III. SMALL-ANGLE X-RAY SCATTERING -- IV. DATA REDUCTION -- V. RESULTS AND DISCUSSION -- VI. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 9 Empirical Fundamental Equations of State for Pure Fluids and Mixtures -- I. INTRODUCTION -- II. EQUATIONS OF STATE -- III. FITTING EQUATIONS OF STATE -- IV. PERFORMANCE OF EQUATIONS OF STATE AND FUTURE CHALLENGES -- V. CONCLUSION -- REFERENCES -- 10 Molecular Simulations to Research Supercritical Fuel Properties -- I. INTRODUCTION -- II. MOLECULAR APPROACH FOR RESEARCHING SUPERCRITICAL FLUIDS -- III. MC SIMULATIONS OF THE PHASE EQUILIBRIUM DIAGRAMS OF -- ALKANE/NITROGEN MIXTURES USING VARIOUS POTENTIALS -- IV. MD SIMULATIONS OF AN -- HEPTANE DROPLET VAPORIZING INTO NITROGEN AT VARIOUS AMBIENT TEMPERATURES AND PRESSURES -- ACKNOWLEDGMENT -- REFERENCES -- 11 Large Eddy Simulations of High-Pressure Jets: Effect of Subgrid-Scale Modeling -- I. INTRODUCTION -- II. GOVERNING EQUATIONS AND NUMERICAL METHOD -- III. NUMERICAL ASPECTS -- IV. CONFIGURATION, BOUNDARY CONDITIONS AND INITIAL CONDITIONS -- V. RESULTS AND DISCUSSION -- VI. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 12 High Pressure Flames with Multicomponent Transport -- I. INTRODUCTION -- II. NONIDEAL FLUIDS -- III. BINARY MIXING LAYERS -- IV. FREELY PROPAGATING PREMIXED FLAMES -- V. STRAINED FLAMES -- VI. TRANSCRITICAL DIFFUSION FLAMES -- VII. CONCLUSION -- REFERENCES -- 13 Large-Eddy Simulation of Cryogenic Jet Injection at Supercritical Pressures -- I. INTRODUCTION -- II. THERMODYNAMICS MODEL. III. CRYOGENIC SINGLE-COMPONENT INJECTION AT SUPERCRITICAL PRESSURE -- IV. CRYOGENIC BINARY COMPONENT INJECTION AT SUPERCRITICAL PRESSURE -- V. CONCLUSION -- ACKNOWLEDGMENTS -- REFERENCES -- 14 Detailed Modeling of Supercritical Jets and Flames -- I. INTRODUCTION -- II. FLUID PROPERTIES IN SUPERCRITICAL ENVIRONMENTS -- III. KINETIC MODELS FOR HIGH-PRESSURE COMBUSTION -- IV. METHODOLOGY FOR ROBUST AND ACCURATE SIMULATIONS OF SUPERCRITICAL FLUIDS WITH LARGE DENSITY CONTRASTS -- V. ROBUST SOLVERS FOR STIFF CHEMISTRY -- VI. LES OF LOX/GH2 SHEAR-COAXIAL JET FLAME AT SUPERCRITICAL PRESSURE -- VII. CONCLUSIONS -- REFERENCES -- 15 Modeling and Simulations of High-Pressure Practical Flows -- I. INTRODUCTION -- II. NUMERICAL TOOLS FOR HIGH-PRESSURE REACTING FLOW SIMULATION -- III. COUPLING REAL-GAS TABULATED THERMOCHEMISTRY AND COMPRESSIBLE LES SOLVER -- IV. SIMULATION OF REACTING AND NONREACTING TURBULENT FLOWS -- V. CONCLUSION -- ACKNOWLEDGMENTS -- APPENDIX A. AEXPRESSION OF THE HEAT CAPACITY AT CONSTANT PRESSURE ( -- APPENDIX B. 2-D CONVECTION OF A MIXTURE FRACTION POCKET [MIXT] -- APPENDIX C. COUPLING THE REAL-GAS TABULATED THERMOCHEMISTRY WITH A LOW-MACH CODE -- REFERENCES -- 16 Large-Eddy Simulation of Liquid Injection and Combustion Processes in High-Pressure Systems -- I. INTRODUCTION -- II. GOVERNING EQUATIONS AND SUBMODEL FORMULATIONS -- III. RESULTS AND DISCUSSION -- IV. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- APPENDIX A. THERMODYNAMIC DERIVATIVES AS FUNCTION OF COMPRESSIBILITY FACTOR FOR THE CUBIC EQUATIONS OF STATE -- APPENDIX B. DEPARTURE FUNCTIONS FOR CUBIC EQUATIONS OF STATE -- REFERENCES -- 17 Simulation of the High-Pressure Combustion Process in Diesel Engines -- NOMENCLATURE -- SUPERSCRIPT -- SUBSCRIPT -- I. INTRODUCTION -- II. DIESEL SPRAY MODEL -- III. GOVERNING EQUATIONS FOR THE FLUID PHASE -- IV. COMBUSTION MODEL. V. CONSTANT-VOLUME COMBUSTION CHAMBER VALIDATIONS -- VI. DIESEL ENGINE SIMULATIONS -- VII. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- Index. |
| Record Nr. | UNINA-9910816598203321 |
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Bellan Josette
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| Reston : , : American Institute of Aeronautics & Astronautics, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran
| High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 |
| Descrizione fisica | 1 online resource (538 p.) |
| Disciplina | 629.134353 |
| Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Propulsion systems
High-speed aeronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-610-7
1-60086-391-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1 Propulsion Systems from Takeoff to High-Speed Flight""; ""Chapter 2 Propulsion System Performance and Integration for High Mach Air Breathing Flight""; ""Chapter 3 Energy Analysis of High-Speed Flight Systems""; ""Chapter 4 Waves and Thermodynamics in High Mach Number Propulsive Ducts""; ""Chapter 5 Turbulent Free Shear Layer Mixing and Combustion""; ""Chapter 6 Turbulent Mixing in Supersonic Combustion Systems""; ""Chapter 7 Mixing and Mixing Enhancement in Supersonic Reacting Flowfields""
""Chapter 8 Study of Combustion and Heat-Exchange Processes in High-Enthalpy Short-Duration Facilities""""Chapter 9 Facility Requirements for Hypersonic Propulsion System Testing""; ""Author Index"" |
| Record Nr. | UNINA-9910457645903321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran
| High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 |
| Descrizione fisica | 1 online resource (538 p.) |
| Disciplina | 629.134353 |
| Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Propulsion systems
High-speed aeronautics |
| ISBN |
1-60086-610-7
1-60086-391-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1 Propulsion Systems from Takeoff to High-Speed Flight""; ""Chapter 2 Propulsion System Performance and Integration for High Mach Air Breathing Flight""; ""Chapter 3 Energy Analysis of High-Speed Flight Systems""; ""Chapter 4 Waves and Thermodynamics in High Mach Number Propulsive Ducts""; ""Chapter 5 Turbulent Free Shear Layer Mixing and Combustion""; ""Chapter 6 Turbulent Mixing in Supersonic Combustion Systems""; ""Chapter 7 Mixing and Mixing Enhancement in Supersonic Reacting Flowfields""
""Chapter 8 Study of Combustion and Heat-Exchange Processes in High-Enthalpy Short-Duration Facilities""""Chapter 9 Facility Requirements for Hypersonic Propulsion System Testing""; ""Author Index"" |
| Record Nr. | UNINA-9910781434203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran
| High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 |
| Descrizione fisica | 1 online resource (538 p.) |
| Disciplina | 629.134353 |
| Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Propulsion systems
High-speed aeronautics |
| ISBN |
1-60086-610-7
1-60086-391-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1 Propulsion Systems from Takeoff to High-Speed Flight""; ""Chapter 2 Propulsion System Performance and Integration for High Mach Air Breathing Flight""; ""Chapter 3 Energy Analysis of High-Speed Flight Systems""; ""Chapter 4 Waves and Thermodynamics in High Mach Number Propulsive Ducts""; ""Chapter 5 Turbulent Free Shear Layer Mixing and Combustion""; ""Chapter 6 Turbulent Mixing in Supersonic Combustion Systems""; ""Chapter 7 Mixing and Mixing Enhancement in Supersonic Reacting Flowfields""
""Chapter 8 Study of Combustion and Heat-Exchange Processes in High-Enthalpy Short-Duration Facilities""""Chapter 9 Facility Requirements for Hypersonic Propulsion System Testing""; ""Author Index"" |
| Record Nr. | UNINA-9910821507003321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Journal of the Global Power and Propulsion Society
| Journal of the Global Power and Propulsion Society |
| Pubbl/distr/stampa | London : , : Veruscript, , 2017- |
| Descrizione fisica | 1 online resource ( : illustrations (black and white, and colour) |
| Disciplina | 621.4 |
| Soggetto topico |
Propulsion systems
Turbomachines Engines |
| Soggetto genere / forma | Periodicals. |
| ISSN | 2515-3080 |
| Formato | Materiale a stampa |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | GPPS journal |
| Record Nr. | UNINA-9910282229603321 |
| London : , : Veruscript, , 2017- | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Journal of the Global Power and Propulsion Society
| Journal of the Global Power and Propulsion Society |
| Pubbl/distr/stampa | London : , : Veruscript, , 2017- |
| Descrizione fisica | 1 online resource ( : illustrations (black and white, and colour) |
| Disciplina | 621.4 |
| Soggetto topico |
Propulsion systems
Turbomachines Engines |
| Soggetto genere / forma | Periodicals. |
| ISSN | 2515-3080 |
| Formato | Materiale a stampa |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | GPPS journal |
| Record Nr. | UNISA-996321770403316 |
| London : , : Veruscript, , 2017- | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
| ||
Nanomaterials in Rocket Propulsion Systems / / edited by Qi-Long Yan [and three others]
| Nanomaterials in Rocket Propulsion Systems / / edited by Qi-Long Yan [and three others] |
| Pubbl/distr/stampa | Amsterdam : , : Elsevier, , 2019 |
| Descrizione fisica | 1 online resource (566 pages) : illustrations |
| Disciplina | 620.115 |
| Soggetto topico |
Propulsion systems
Rocket engines - Materials Nanostructured materials |
| ISBN |
0-12-813909-9
0-12-813908-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | The prospects of using nanoenergetic materials in solid rocket propulsion / Vladimir E. Zarko -- Review on nanoexplosive materials / Bing Gao, Zhiqiang Qiao and Guangcheng Yang -- Intensive energetic materials containing two-dimensional nanostructures as building blocks / Qi-Long Yan, Michael Gozin, Pei-Jin Liu and Guo-Qiang He -- Preparation, characterization, and application of superthermites in solid propellant / Ting An, Wen-Gang Qu, Yan-Jing Yang, Feng-qi Zhao and Qi-Long Yan -- Aluminum powders for energetics : properties and oxidation behavior / A.A. Gromov, A. Yu Nalivaiko, V.P. Tarasov, S.V. Zmanovsky, A.N. Arnautov, A.V. Sergienko, and K.B. Larionov -- Nanoenergetic ingredients to augment solid rocket propulsion / Luigi T. De Luca -- Performance of composite solid propellant containing nanosized metal particles / WeiQiang Pang, Luigi T. De. Luca, Ke Wang, XiaoLong Fu, JunQiang Li, HuiZXiang Xu, XueZhong Fan and Huan Li -- Effect if ammonium perchlorate particle size on flow, ballistic, and mechanical properties of composite propellant / Jauhari Ashish, Gharde Swaroop and Kandasubramanian Balasubramanian -- New developments in composite propellants catalysis : from nanoparticles to metallo-polyurethanes / Carlos Hortelano and José Luis de la Fuente -- Chemical propulsion of microthrusters / Ruiqi Shen, Yinghua Ye, Chengling Wang, Chengbo Ru and Ji Dai -- Chemical propulsion of microthrusters / Ruiqi Shen, Yinghua Ye, Chengling Want, Chengbo Ru and Ji Dai -- Integrated Micropropulsion systems with nanoenergetic propellants / Mkhitar Hobosyan, Sergey E. Lyshevski and Karen S. Martirosyan -- Polymer nanocomposite ablative technologies for solid rocket motors / Joseph H. Koo and Jon Langston -- Nanotube/nanowire--toughened carbon/carbon composites and their coatings / Qiang Song, Lei Zhuang and Qian-Gang Fu -- An introduction to ablative materials and high-temperature testing protocols / Marco Rallini, Maurizio Natali and Luigi Torre. |
| Record Nr. | UNINA-9910583470503321 |
| Amsterdam : , : Elsevier, , 2019 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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