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Combustion of lox with H₂₍g₎ under subcritical, critical and supercritical conditions (task 1) and experimental observation of dense spray and mixing of impinging jets (task 2) [[electronic resource] ] : semi-annual report / / prepared by K.K. Kou ... [et al
| Combustion of lox with H₂₍g₎ under subcritical, critical and supercritical conditions (task 1) and experimental observation of dense spray and mixing of impinging jets (task 2) [[electronic resource] ] : semi-annual report / / prepared by K.K. Kou ... [et al |
| Pubbl/distr/stampa | University Park, PA : , : Propulsion Engineering Research Center, Pennsylvania State University |
| Descrizione fisica | 1 online resource (vi, 55 pages) : illustrations |
| Altri autori (Persone) | KuoKenneth K |
| Collana | [NASA contractor report] |
| Soggetto topico |
Cavitation flow
Combustion physics Hydrogen Impingement Liquid oxygen Mathematical models Spray characteristics Sprayers Thermodynamic equilibrium |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Combustion of lox with H₂₍g₎ under subcritical, critical and supercritical conditions |
| Record Nr. | UNINA-9910702001403321 |
| University Park, PA : , : Propulsion Engineering Research Center, Pennsylvania State University | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo
| Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
| Descrizione fisica | 1 online resource (665 p.) |
| Disciplina | 629.47/52 |
| Altri autori (Persone) |
ChiaveriniMartin J <1968-> (Martin John)
KuoKenneth K |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Hybrid propellant rockets
Rocket engines - Combustion Rockets (Aeronautics) - Fuel |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-687-5
1-60086-468-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Acknowledgements""; ""Table of Contents""; ""Chapter 1. Overview and History of Hybrid Rocket Propulsion""; ""Chapter 2. Review of Solid-Fuel Regression Rate Behavior in Classical and Nonclassical Hybrid Rocket Motors""; ""Chapter 3. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 1: Mechanisms""; ""Chapter 4. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 2: Measurement Techniques""; ""Chapter 5. Analytical Models for Hybrid Rockets""; ""Chapter 6. Vortex Injection Hybrid Rockets""
""Chapter 7. High-Speed Flow Effects in Hybrid Rockets""""Chapter 8. Computational Fluid Dynamics Modeling of Hybrid Rocket Flowfields""; ""Chapter 9. Combustion Instability and Transient Behavior in Hybrid Rocket Motors""; ""Chapter 10. Metals, Energetic Additives, and Special Binders Used in Solid Fuels for Hybrid Rockets""; ""Chapter 11. Hydrogen Peroxide, Hydroxyl Ammonium Nitrate, and Other Storable Oxidizers""; ""Chapter 12. Similarity and Scaling Effects in Hybrid Rocket Motors""; ""Chapter 13. Large-Scale Hybrid Motor Testing"" ""Chapter 14. Flight Testing of Hybrid-Powered Vehicles""""Chapter 15. Challenges of Hybrid Rocket Propulsion in the 21st Century""; ""Index"" |
| Record Nr. | UNINA-9910456604703321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo
| Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
| Descrizione fisica | 1 online resource (665 p.) |
| Disciplina | 629.47/52 |
| Altri autori (Persone) |
ChiaveriniMartin J <1968-> (Martin John)
KuoKenneth K |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Hybrid propellant rockets
Rocket engines - Combustion Rockets (Aeronautics) - Fuel |
| ISBN |
1-60086-687-5
1-60086-468-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Acknowledgements""; ""Table of Contents""; ""Chapter 1. Overview and History of Hybrid Rocket Propulsion""; ""Chapter 2. Review of Solid-Fuel Regression Rate Behavior in Classical and Nonclassical Hybrid Rocket Motors""; ""Chapter 3. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 1: Mechanisms""; ""Chapter 4. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 2: Measurement Techniques""; ""Chapter 5. Analytical Models for Hybrid Rockets""; ""Chapter 6. Vortex Injection Hybrid Rockets""
""Chapter 7. High-Speed Flow Effects in Hybrid Rockets""""Chapter 8. Computational Fluid Dynamics Modeling of Hybrid Rocket Flowfields""; ""Chapter 9. Combustion Instability and Transient Behavior in Hybrid Rocket Motors""; ""Chapter 10. Metals, Energetic Additives, and Special Binders Used in Solid Fuels for Hybrid Rockets""; ""Chapter 11. Hydrogen Peroxide, Hydroxyl Ammonium Nitrate, and Other Storable Oxidizers""; ""Chapter 12. Similarity and Scaling Effects in Hybrid Rocket Motors""; ""Chapter 13. Large-Scale Hybrid Motor Testing"" ""Chapter 14. Flight Testing of Hybrid-Powered Vehicles""""Chapter 15. Challenges of Hybrid Rocket Propulsion in the 21st Century""; ""Index"" |
| Record Nr. | UNINA-9910780786303321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo
| Fundamentals of hybrid rocket combustion and propulsion [[electronic resource] /] / edited by Martin J. Chiaverini, Kenneth K. Kuo |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
| Descrizione fisica | 1 online resource (665 p.) |
| Disciplina | 629.47/52 |
| Altri autori (Persone) |
ChiaveriniMartin J <1968-> (Martin John)
KuoKenneth K |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Hybrid propellant rockets
Rocket engines - Combustion Rockets (Aeronautics) - Fuel |
| ISBN |
1-60086-687-5
1-60086-468-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Acknowledgements""; ""Table of Contents""; ""Chapter 1. Overview and History of Hybrid Rocket Propulsion""; ""Chapter 2. Review of Solid-Fuel Regression Rate Behavior in Classical and Nonclassical Hybrid Rocket Motors""; ""Chapter 3. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 1: Mechanisms""; ""Chapter 4. Solid-Fuel Pyrolysis Phenomena and Regression Rate, Part 2: Measurement Techniques""; ""Chapter 5. Analytical Models for Hybrid Rockets""; ""Chapter 6. Vortex Injection Hybrid Rockets""
""Chapter 7. High-Speed Flow Effects in Hybrid Rockets""""Chapter 8. Computational Fluid Dynamics Modeling of Hybrid Rocket Flowfields""; ""Chapter 9. Combustion Instability and Transient Behavior in Hybrid Rocket Motors""; ""Chapter 10. Metals, Energetic Additives, and Special Binders Used in Solid Fuels for Hybrid Rockets""; ""Chapter 11. Hydrogen Peroxide, Hydroxyl Ammonium Nitrate, and Other Storable Oxidizers""; ""Chapter 12. Similarity and Scaling Effects in Hybrid Rocket Motors""; ""Chapter 13. Large-Scale Hybrid Motor Testing"" ""Chapter 14. Flight Testing of Hybrid-Powered Vehicles""""Chapter 15. Challenges of Hybrid Rocket Propulsion in the 21st Century""; ""Index"" |
| Record Nr. | UNINA-9910806267303321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield
| Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 |
| Descrizione fisica | 1 online resource (906 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
KuoKenneth K
SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-567-4
1-60086-348-5 1-61583-527-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title; Copyright; Table of Contents; Authors; Preface; Acknowledgments; Chapter 1. Survey of Rocket Propellants and Their Combustion Characteristics; Performance of a Solid-Propellant Rocket Motor; Stable Combustion of a Rocket Motor; Temperature Sensitivity of Burning Rate; Thermochemical Properties of Propellant Ingredients; Thermochemical Properties of Propellant Combustion Products; Combustion Processes of Various Types of Solid Propellants; Double-Base Propellants; Ammonium Perchlorate Composite Propellants; Composite Modified Double-Base Propellants
Nitramine Composite PropellantsBurning Rate Controlling Factors of Solid Propellants; Combustion Characteristics Required for Solid Propellants and General Description of the Combustion Wave; Heat-Transfer Mechanism in Combustion Waves; Heat Transfer in Solid Phase; Heat Transfer in Gas Phase; Reaction Rate in Gas Phase; Burning Rate of Solid Propellant Calculated by a Simplified Gas-Phase Model; Chapter 2. Chemistry of Ignition and Combustion of Ammonium-Perchlorate-Based Propellants; Chemistry of Ignition; Sequence of Ignition; Theories of Ignition; Role of Oxidizer and Binder Effect of PressureEffect of Oxidizing Atmosphere; Ignition of Composite Propellant Fuels by HClO(sub[4]) Vapor; Preignition Reactions; Effect of Catalysts on Ignition; Chemistry of Combustion; Introduction to Combustion Mechanism; Surface Reactions; Subsurface Reactions; Gas-Phase Reactions; Effect of Catalysts on Propellant Combustion; Future Research Directions; Chapter 3. The Thermal Behavior of Cyclotrimethylenetrinitramine (RDX) and Cyclotetramethylenetetranitramine (HMX); Crystallography; Sublimation of HMX; Decomposition of the Solid RDX and HMX; Liquefaction; Decomposition of Liquid Pyrolysis of HMXShock Tube Studies; Ignition of HMX; Self-Deflagration of HMX and RDX; Self-Deflagration Rate as a Function of Pressure; Self-Deflagration Rate as a Function of Pressure and Initial Sample Temperature; Surface Structure of Self-Deflagrating HMX; Chapter 4. Chemistry of Nitrate Ester and Nitramine Propellants; Decomposition of Nitrocellulose; Kinetics of Nitrocellulose Decomposition; Products and Mechanism of Nitrocellulose Decomposition; Plasticizers and Stabilizers in Nitrocellulose Decomposition; Catalysis of Nitrate Ester Propellants; Decomposition of Nitramines Kinetics of HMX and RDX DecompositionProducts and Mechanism of HMX and RDX Pyrolysis; Catalysis of Nitramine Propellants; Flame Zone Chemistry; Chapter 5. Solid-Propellant Ignition Theories and Experiments; Introduction; Radiant Energy Ignition Sources; Shock Tube and Other Ignition Experiments; Theoretical Models of Solid-Propellant Ignition and Related Theory; Comments on Solution Methods; Solid-Phase Reaction Mechanism Theory; Theory of Ignition by Heterogeneous Reaction with External Oxidizer; Gas-Phase Theory of Solid-Propellant Ignition; Gas-Phase Theory-Shock Tube Cases Gas-Phase Theory-Radiant Heat Input |
| Record Nr. | UNINA-9910458920903321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield
| Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 |
| Descrizione fisica | 1 online resource (906 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
KuoKenneth K
SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| ISBN |
1-60086-567-4
1-60086-348-5 1-61583-527-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title; Copyright; Table of Contents; Authors; Preface; Acknowledgments; Chapter 1. Survey of Rocket Propellants and Their Combustion Characteristics; Performance of a Solid-Propellant Rocket Motor; Stable Combustion of a Rocket Motor; Temperature Sensitivity of Burning Rate; Thermochemical Properties of Propellant Ingredients; Thermochemical Properties of Propellant Combustion Products; Combustion Processes of Various Types of Solid Propellants; Double-Base Propellants; Ammonium Perchlorate Composite Propellants; Composite Modified Double-Base Propellants
Nitramine Composite PropellantsBurning Rate Controlling Factors of Solid Propellants; Combustion Characteristics Required for Solid Propellants and General Description of the Combustion Wave; Heat-Transfer Mechanism in Combustion Waves; Heat Transfer in Solid Phase; Heat Transfer in Gas Phase; Reaction Rate in Gas Phase; Burning Rate of Solid Propellant Calculated by a Simplified Gas-Phase Model; Chapter 2. Chemistry of Ignition and Combustion of Ammonium-Perchlorate-Based Propellants; Chemistry of Ignition; Sequence of Ignition; Theories of Ignition; Role of Oxidizer and Binder Effect of PressureEffect of Oxidizing Atmosphere; Ignition of Composite Propellant Fuels by HClO(sub[4]) Vapor; Preignition Reactions; Effect of Catalysts on Ignition; Chemistry of Combustion; Introduction to Combustion Mechanism; Surface Reactions; Subsurface Reactions; Gas-Phase Reactions; Effect of Catalysts on Propellant Combustion; Future Research Directions; Chapter 3. The Thermal Behavior of Cyclotrimethylenetrinitramine (RDX) and Cyclotetramethylenetetranitramine (HMX); Crystallography; Sublimation of HMX; Decomposition of the Solid RDX and HMX; Liquefaction; Decomposition of Liquid Pyrolysis of HMXShock Tube Studies; Ignition of HMX; Self-Deflagration of HMX and RDX; Self-Deflagration Rate as a Function of Pressure; Self-Deflagration Rate as a Function of Pressure and Initial Sample Temperature; Surface Structure of Self-Deflagrating HMX; Chapter 4. Chemistry of Nitrate Ester and Nitramine Propellants; Decomposition of Nitrocellulose; Kinetics of Nitrocellulose Decomposition; Products and Mechanism of Nitrocellulose Decomposition; Plasticizers and Stabilizers in Nitrocellulose Decomposition; Catalysis of Nitrate Ester Propellants; Decomposition of Nitramines Kinetics of HMX and RDX DecompositionProducts and Mechanism of HMX and RDX Pyrolysis; Catalysis of Nitramine Propellants; Flame Zone Chemistry; Chapter 5. Solid-Propellant Ignition Theories and Experiments; Introduction; Radiant Energy Ignition Sources; Shock Tube and Other Ignition Experiments; Theoretical Models of Solid-Propellant Ignition and Related Theory; Comments on Solution Methods; Solid-Phase Reaction Mechanism Theory; Theory of Ignition by Heterogeneous Reaction with External Oxidizer; Gas-Phase Theory of Solid-Propellant Ignition; Gas-Phase Theory-Shock Tube Cases Gas-Phase Theory-Radiant Heat Input |
| Record Nr. | UNINA-9910792120503321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield
| Fundamentals of solid-propellant combustion [[electronic resource] /] / edited by Kenneth K. Kuo, Martin Summerfield |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 |
| Descrizione fisica | 1 online resource (906 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
KuoKenneth K
SummerfieldMartin |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Solid propellants - Combustion |
| ISBN |
1-60086-567-4
1-60086-348-5 1-61583-527-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title; Copyright; Table of Contents; Authors; Preface; Acknowledgments; Chapter 1. Survey of Rocket Propellants and Their Combustion Characteristics; Performance of a Solid-Propellant Rocket Motor; Stable Combustion of a Rocket Motor; Temperature Sensitivity of Burning Rate; Thermochemical Properties of Propellant Ingredients; Thermochemical Properties of Propellant Combustion Products; Combustion Processes of Various Types of Solid Propellants; Double-Base Propellants; Ammonium Perchlorate Composite Propellants; Composite Modified Double-Base Propellants
Nitramine Composite PropellantsBurning Rate Controlling Factors of Solid Propellants; Combustion Characteristics Required for Solid Propellants and General Description of the Combustion Wave; Heat-Transfer Mechanism in Combustion Waves; Heat Transfer in Solid Phase; Heat Transfer in Gas Phase; Reaction Rate in Gas Phase; Burning Rate of Solid Propellant Calculated by a Simplified Gas-Phase Model; Chapter 2. Chemistry of Ignition and Combustion of Ammonium-Perchlorate-Based Propellants; Chemistry of Ignition; Sequence of Ignition; Theories of Ignition; Role of Oxidizer and Binder Effect of PressureEffect of Oxidizing Atmosphere; Ignition of Composite Propellant Fuels by HClO(sub[4]) Vapor; Preignition Reactions; Effect of Catalysts on Ignition; Chemistry of Combustion; Introduction to Combustion Mechanism; Surface Reactions; Subsurface Reactions; Gas-Phase Reactions; Effect of Catalysts on Propellant Combustion; Future Research Directions; Chapter 3. The Thermal Behavior of Cyclotrimethylenetrinitramine (RDX) and Cyclotetramethylenetetranitramine (HMX); Crystallography; Sublimation of HMX; Decomposition of the Solid RDX and HMX; Liquefaction; Decomposition of Liquid Pyrolysis of HMXShock Tube Studies; Ignition of HMX; Self-Deflagration of HMX and RDX; Self-Deflagration Rate as a Function of Pressure; Self-Deflagration Rate as a Function of Pressure and Initial Sample Temperature; Surface Structure of Self-Deflagrating HMX; Chapter 4. Chemistry of Nitrate Ester and Nitramine Propellants; Decomposition of Nitrocellulose; Kinetics of Nitrocellulose Decomposition; Products and Mechanism of Nitrocellulose Decomposition; Plasticizers and Stabilizers in Nitrocellulose Decomposition; Catalysis of Nitrate Ester Propellants; Decomposition of Nitramines Kinetics of HMX and RDX DecompositionProducts and Mechanism of HMX and RDX Pyrolysis; Catalysis of Nitramine Propellants; Flame Zone Chemistry; Chapter 5. Solid-Propellant Ignition Theories and Experiments; Introduction; Radiant Energy Ignition Sources; Shock Tube and Other Ignition Experiments; Theoretical Models of Solid-Propellant Ignition and Related Theory; Comments on Solution Methods; Solid-Phase Reaction Mechanism Theory; Theory of Ignition by Heterogeneous Reaction with External Oxidizer; Gas-Phase Theory of Solid-Propellant Ignition; Gas-Phase Theory-Shock Tube Cases Gas-Phase Theory-Radiant Heat Input |
| Record Nr. | UNINA-9910818063003321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Recent advances in spray combustion [[electronic resource] ] : spray atomization and drop burning phenomena. Volume I / / edited by Kenneth K. Kuo
| Recent advances in spray combustion [[electronic resource] ] : spray atomization and drop burning phenomena. Volume I / / edited by Kenneth K. Kuo |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 |
| Descrizione fisica | 1 online resource (518 p.) |
| Altri autori (Persone) | KuoKenneth K |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Combustion
Combustion engineering Spraying |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-641-7
1-60086-422-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Subject Area 1. Drop Sizing Techniques""; ""Chapter 1. Review of Principles of Optical Techniques for Particle Size Measurements""; ""Chapter 2. Theory and Measurement of the Multipoint Statistics of Sprays""; ""Chapter 3. Intra- and Interlaboratory Experiments to Assess Performance of Phase Doppler Interferometry""; ""Subject Area 2. Breakup Processes of Liquid Jets and Sheets""; ""Chapter 4. Regimes of Jet Breakup and Breakup Mechanisms (Physical Aspects)""
""Chapter 5. Regimes of Jet Breakup and Breakup Mechanisms (Mathematical Aspects)""""Chapter 6. Aerothermodynamic Effects on Liquid Jet Breakup in Two-Fluid Fuel Nozzles""; ""Chapter 7. Effect of Internal Flow Conditions Inside Injector Nozzles on Jet Breakup Processes""; ""Chapter 8. Measurement of Core Structure of Coaxial Jets Under Cold-Flow and Hot-Fire Conditions""; ""Chapter 9. Theoretical Modeling of Liquid Jet and Sheet Breakup Processes""; ""Chapter 10. Atomization of Liquid Sheets""; ""Subject Area 3. Dense Spray Behavior"" ""Chapter 11. Nonintrusive Measurement of the Structure of Dense Sprays""""Chapter 12. Measurement of Drop Sizes in Unsteady Dense Sprays""; ""Chapter 13. Deliberations on the Dynamics and Core Structure of Reacting Sprays at Elevated Pressures""; ""Chapter 14. Generation, Vaporization, and Combustion of Droplet Arrays and Streams""; ""Chapter 15. Fundamentals of Dynamics and Evaporation in Clusters of Drops Embedded into Vortices""; ""Chapter 16. Far-Field Coalescence Effects in Polydisperse Spray Diffusion Flames"" ""Subject Area 4. Supercritical Evaporation and Burning of Liquid Propellants""""Chapter 17. Droplet Behavior at Supercritical Conditions""; ""Chapter 18. Supercritical Evaporation and Combustion of Liquid Oxygen in an Axisymmetric Configuration""; ""Chapter 19. Modeling of Atomization and Secondary Breakup from First Principles""; ""Author Index"" |
| Record Nr. | UNINA-9910457255603321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Recent advances in spray combustion [[electronic resource] ] : spray combustion measurements and model simulation. Volume II / / edited by Kenneth K. Kuo
| Recent advances in spray combustion [[electronic resource] ] : spray combustion measurements and model simulation. Volume II / / edited by Kenneth K. Kuo |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 |
| Descrizione fisica | 1 online resource (466 p.) |
| Altri autori (Persone) | KuoKenneth K |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Combustion
Combustion engineering Spraying |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-643-3
1-60086-424-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Subject Area 1. Spray Combustion Measurements""; ""Chapter 1. Continuous- and Dispersed-Phase Structure of Pressure-Atomized Sprays""; ""Chapter 2. Behavior of Droplets in Pressure-Atomized Fuel Sprays with Coflowing Air Swirl""; ""Chapter 3. Spray Diagnostics with Lasing and Stimulated Raman Scattering""; ""Chapter 4. Feasibility of Droblet Size and Concentration Measurements in a Hypergolic Prepellant Burning Spray""; ""Chapter 5. Laser Sheet Visualization of Spray Structure""
""Chapter 6. Use of Fluorescence Methods for Measurement of Droplet and Vapor Temperatures""""Chapter 7. Assessing the Physics of Spray Behavior in Complex Combustion Systems""; ""Chapter 8. Structure of a Coflow Laminar Spray Diffusion Flame""; ""Chapter 9. Coaxial Airblast Atomizers with Swirling Air Stream""; ""Chapter 10. Pressure Oscillation Effects on Jet Breakup""; ""Subject Area 2. Spray Combustion Modeling and Numerical Simulation""; ""Chapter 11. Simulation of High-Pressure Spray Field Dynamics""; ""Chapter 12. Numerical Simulation of Deformed Droplet Dynamics and Evaporation"" ""Subject Area 3. Instability of Liquid Fueled Combustion Systems""""Chapter 13. Numerical Simulation of High-Frequency Combustion Instabilities in Liquid Rocket Engines""; ""Chapter 14. Performance and Stability Characterization of Liquid Oxygen/Kerosene Injectors at Aerojet""; ""Chapter 15. Acoustic Sensitivity Measurements of Injectors in a Small Liquid Propellant Rocket Engine""; ""Subject Area 4. Spray Combustion in Certain Practical Systems""; ""Chapter 16. Spray Combustion Processes in Internal Combustion Engines"" ""Chapter 17. Spray Combustion Processes in Regenerative Liquid Propellant Guns""""Author Index"" |
| Record Nr. | UNINA-9910457203503321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Recent advances in spray combustion [[electronic resource] ] : spray combustion measurements and model simulation. Volume II / / edited by Kenneth K. Kuo
| Recent advances in spray combustion [[electronic resource] ] : spray combustion measurements and model simulation. Volume II / / edited by Kenneth K. Kuo |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 |
| Descrizione fisica | 1 online resource (466 p.) |
| Altri autori (Persone) | KuoKenneth K |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Combustion
Combustion engineering Spraying |
| ISBN |
1-60086-643-3
1-60086-424-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Subject Area 1. Spray Combustion Measurements""; ""Chapter 1. Continuous- and Dispersed-Phase Structure of Pressure-Atomized Sprays""; ""Chapter 2. Behavior of Droplets in Pressure-Atomized Fuel Sprays with Coflowing Air Swirl""; ""Chapter 3. Spray Diagnostics with Lasing and Stimulated Raman Scattering""; ""Chapter 4. Feasibility of Droblet Size and Concentration Measurements in a Hypergolic Prepellant Burning Spray""; ""Chapter 5. Laser Sheet Visualization of Spray Structure""
""Chapter 6. Use of Fluorescence Methods for Measurement of Droplet and Vapor Temperatures""""Chapter 7. Assessing the Physics of Spray Behavior in Complex Combustion Systems""; ""Chapter 8. Structure of a Coflow Laminar Spray Diffusion Flame""; ""Chapter 9. Coaxial Airblast Atomizers with Swirling Air Stream""; ""Chapter 10. Pressure Oscillation Effects on Jet Breakup""; ""Subject Area 2. Spray Combustion Modeling and Numerical Simulation""; ""Chapter 11. Simulation of High-Pressure Spray Field Dynamics""; ""Chapter 12. Numerical Simulation of Deformed Droplet Dynamics and Evaporation"" ""Subject Area 3. Instability of Liquid Fueled Combustion Systems""""Chapter 13. Numerical Simulation of High-Frequency Combustion Instabilities in Liquid Rocket Engines""; ""Chapter 14. Performance and Stability Characterization of Liquid Oxygen/Kerosene Injectors at Aerojet""; ""Chapter 15. Acoustic Sensitivity Measurements of Injectors in a Small Liquid Propellant Rocket Engine""; ""Subject Area 4. Spray Combustion in Certain Practical Systems""; ""Chapter 16. Spray Combustion Processes in Internal Combustion Engines"" ""Chapter 17. Spray Combustion Processes in Regenerative Liquid Propellant Guns""""Author Index"" |
| Record Nr. | UNINA-9910781700403321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
