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Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang
| Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang |
| Autore | Wang Zhen-Guo |
| Pubbl/distr/stampa | Singapore : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (395 p.) |
| Disciplina | 629.47522 |
| Soggetto topico |
Liquid propellant rockets
Liquid propellant rocket engines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-118-89005-1
1-118-89004-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation |
| Record Nr. | UNINA-9910136758203321 |
Wang Zhen-Guo
|
||
| Singapore : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang
| Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang |
| Autore | Wang Zhen-Guo |
| Pubbl/distr/stampa | Singapore : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (395 p.) |
| Disciplina | 629.47522 |
| Soggetto topico |
Liquid propellant rockets
Liquid propellant rocket engines |
| ISBN |
1-118-89005-1
1-118-89004-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation |
| Record Nr. | UNINA-9910830290403321 |
|
Wang Zhen-Guo
|
||
| Singapore : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang
| Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (580 p.) |
| Disciplina | 629.47522 |
| Altri autori (Persone) | YoungVigor |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-637-9
1-60086-418-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. |
| Record Nr. | UNINA-9910457165203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang
| Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (580 p.) |
| Disciplina | 629.47522 |
| Altri autori (Persone) | YoungVigor |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion |
| ISBN |
1-60086-637-9
1-60086-418-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. |
| Record Nr. | UNINA-9910781420203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rocket engine combustion instability / / edited by William E. Anderson and Vigor Yang
| Liquid rocket engine combustion instability / / edited by William E. Anderson and Vigor Yang |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (580 p.) |
| Disciplina | 629.47522 |
| Altri autori (Persone) | YoungVigor |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion |
| ISBN |
1-60086-637-9
1-60086-418-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. |
| Record Nr. | UNINA-9910957334203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Modern engineering for design of liquid-propellant rocket engines / / Dieter K. Huzel and David H. Huang ; revised, updated, and enlarged by Harry Arbit ... [et al.]
| Modern engineering for design of liquid-propellant rocket engines / / Dieter K. Huzel and David H. Huang ; revised, updated, and enlarged by Harry Arbit ... [et al.] |
| Autore | Huzel Dieter K |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 |
| Descrizione fisica | 425 p. : ill |
| Disciplina | 629.47522 |
| Altri autori (Persone) |
HuangDavid H. <1920->
ArbitHarry |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Liquid propellant rocket engines - Design and construction |
| ISBN |
1-60086-619-0
1-60086-400-7 1-60119-227-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover -- Title -- Copyright -- Foreword -- Preface -- Table of Contents -- Chapter 1. Introduction to Liquid-Propellant Rocket Engines -- 1.1 Basic Elements of a Liquid-Propellant Rocket Engine -- 1.2 Generation of Thrust -- 1.3 Gas-Flow Processes in the Combustion Chamber and Nozzle -- The Perfect Gas Law -- Principle of Conservation of Energy -- Principle of Conservation of Matter -- The Isentropic Flow Process -- Gas Flow Through Liquid-Propellant Rocket Combustion Chambers -- Gas Flow Through Rocket Nozzles -- 1.4 Performance Parameters of a Liquid-Propellant Rocket Engine -- Thrust-Chamber Specific Impulse (I[sub(s)])tc -- Characteristic Velocity c* -- Thrust Coefficient C[sub(f)] -- Summary of the Influence of pa, ε, γ, R, and (p[sub(c)])ns on Engine Performance -- Correction Factors and Magnitudes of Engine Performance Parameters -- 1.5 Liquid Propellants -- Monopropellants -- Bipropellants -- Cryogenic Propellants -- Storable Liquid Propellants -- Additives for Liquid Propellants -- Optimum Mixture Ratio -- Density Impulse -- Selection of Liquid Propellants -- Liquid-Propellant Performance and Physical Properties -- Chapter 2. Engine Requirements and Preliminary Design Analyses -- 2.1 Introduction -- 2.2 Major Rocket-Engine Design Parameters -- Thrust Level -- Performance -- Duration -- Mixture Ratio -- Weight -- Envelope (Size) -- Reliability -- Cost -- Availability (Scheduling) -- 2.3 Mission Requirements -- Typical Mission Goals -- Typical Vehicle Requirement Optimization -- 2.4 Engine Preliminary Design -- Engine System and Component Concepts -- Preliminary Design Optimization -- 2.5 Design Philosophy -- The Importance of Design Quality -- Systems Analysis and Design Layout -- Stress Analysis -- Selection of Materials -- Chapter 3. Introduction to Sample Calculations -- 3.1 Approach -- 3.2 A-1 Stage Engine.
General Engine-System Description -- System Operation -- 3.3 A-2 Stage Engine -- General Engine-System Description -- System Operation -- Starting Sequence -- Cutoff Sequence -- 3.4 A-3 Stage Engine -- General Engine-System Description -- System Operation -- 3.5 A-4 Stage Engine -- General Engine System Description -- System Operation -- Chapter 4. Design of Thrust Chambers and Other Combustion Devices -- 4.1 Basic Thrust-Chamber Elements -- 4.2 Thrust-Chamber Performance Parameters -- Specific Impulse I[sub(s)] (s) -- Characteristic Velocity c* (ft/s) -- Thrust Coefficient C[sub(f)] (Dimensionless) -- Performance Calculation -- 4.3 Thrust-Chamber Configuration Layout -- Combustion-Chamber Volume -- Combustion-Chamber Shape -- Nozzle Expansion Area Ratio -- Nozzle Shape -- Clustered-Nozzle Concepts -- Alternate Solution -- 4.4 Thrust-Chamber Cooling -- Cooling Techniques and Selection -- Gas-Side Heat Transfer -- Regenerative Cooling -- Coolant-Side Heat Transfer -- Wall Design Considerations -- Tubular-Wall Thrust-Chamber Design -- Coaxial-Shell Thrust-Chamber Design -- Pressure Drop in Cooling Passages -- Channel-Wall Design -- Dump Cooling -- Film Cooling -- Liquid-Film Cooling -- Gaseous-Film Cooling -- Mixture-Ratio Bias -- Transpiration Cooling -- Ablative Cooling -- Radiation Cooling -- Heat-Sink Cooling -- Combined Cooling Methods -- 4.5 Injector Design -- Injector Design Issues -- Combustion Stability -- Manifolds -- Manifold Types -- Injection Elements -- Nonimpinging Elements -- Unlike-Impinging Elements -- Like-Impinging Elements -- Other Element Types -- Throttling -- Injection Pressure Drop and Orifice Sizing -- Experimental Evaluation of Injector Designs -- Analytical Models -- 4.6 Gas-Generating Devices -- Solid-Propellant Gas Generators -- Liquid-Monopropellant Gas Generators -- Liquid-Bipropellant Gas Generators. Thrust-Chamber Gas-Tapoff Systems -- 4.7 Ignition Devices -- Igniters -- Hypergolic Igniters -- Ignition Detection -- 4.8 Combustion Instability -- Types of Instability -- Intrinsic Acoustic Instabilities -- Injection-Coupled Acoustic Instability -- Low-Frequency Instabilities -- Prevention of Triggering Mechanisms -- Propellant-Feed System Design -- Combustion-Chamber Design -- Injector Design -- Propellant Combination and Mixture Ratio -- Engine-System Operating Characteristics -- Application of Damping Devices -- Injector Baffles -- Chamber Divergent Wall Gap -- Acoustic Cavities and Liners -- Stability Rating -- Feed-System Disturbances -- Combustion-Chamber Disturbances -- Spontaneous-Instability Methods -- Instrumentation -- Chapter 5. Design of Gas-Pressurized Propellant Feed Systems -- 5.1 Determination of Pressurant Requirements -- Required System Data -- Factors Influencing Pressurant Requirements -- Design Calculations of Pressurant Requirements -- 5.2 Stored-Gas Systems -- Commonly Used Configurations -- Calculations for Stored-Gas Requirements -- Design of Stored-Gas System Components -- Tanks -- Pressure Regulators -- Thrust-Chamber Heat Exchangers -- 5.3 Propellant-Evaporation Systems -- Pump-Fed Propellant Feed Systems -- Gas-Pressurized Propellant Feed Systems -- 5.4 Inert-Gas-Evaporation Systems -- 5.5 Chemical-Reaction Systems -- Solid-Propellant Gas Generators -- Liquid-Propellant Gas Generator -- Direct Injection into Propellant Tank -- 5.6 Selection of Pressurization -- Chapter 6. Design of Turbopump Propellant Feed Systems -- 6.1 Elements of Turbopump-Fed Systems -- Propellant Pumps -- Turbines -- Turbine Power Sources -- Turbopump-Drive Arrangements -- Description of Developed Turbopump Systems -- 6.2 Turbopump System Performance and Design Parameters -- Turbopump System Performance -- Turbopump System Design Parameters. 6.3 Inducer Design -- 6.4 Design of Centrifugal Pumps -- General Design Procedures -- Operating Principles of the Centrifugal Impeller -- Centrifugal-Impeller Design Elements -- Design of Casings -- Balancing the Axial Thrust of Centrifugal Pumps -- 6.5 Design of Axial-Flow Pumps -- Basic Assumptions for Axial-Flow Pumps -- Operation of the Impeller Rotor -- Function of the Stator -- Design of Impeller Rotors and Stators -- Diffusion and Retardation Factors -- Design of Casings for Axial Pumps -- Balancing the Axial Thrust of Multistage Axial Pumps -- 6.6 Turbine Design -- General Design Procedure -- Design of Turbine Nozzles -- Design of Turbine Rotor Blades -- Design of Single-Stage, Two-Rotor, Velocity-Compounded Impulse Turbines -- Design of Two-Stage, Two-Rotor, Pressure-Compounded Impulse Turbine -- Design of Two-Stage, Two-Rotor, Low Reaction Turbine -- 6.7 Turbopump Rotordynamics and Mechanical Elements -- Rotordynamics -- Turbopump Bearing Design -- Dynamic-Seal Design -- Turbopump Gear Design -- 6.8 Design Layout of Turbopump Assemblies -- 6.9 References -- Chapter 7. Design of Rocket-Engine Control and Condition-Monitoring Systems -- 7.1 CCM-Into a New Era -- Basic Liquid-Propellant-Engine Control Systems -- Engine Thrust-Level Control -- Propellant-Mixture-Ratio and Propellant-Utilization Control -- Thrust-Vector Control -- CCM Concept and Preliminary Design Development -- Control Methods -- Control-Law Development -- 7.2 Design of Fluid-Flow-Control Devices -- Design Considerations for Fluid-Flow-Control Components -- Design of Dynamic Seals for Fluid-Control Components -- Design of Seating Closures for Fluid-Control Components -- Design of Propellant Valves -- Design of Control Pilot Valves -- Design of Servovalves -- Design of Gas-Pressure Regulators -- Design of Liquid-Flow and Pressure Regulators -- Design of Pressure-Relief Valves. Design of Miscellaneous Fluid-Flow-Control Components -- 7.3 Design of Instrumentation and Harnesses -- Engine Instrumentation -- Principal Types of Instrumentation -- Instrumentation Installation -- Engine Harnesses -- Design Considerations -- 7.4 Avionics Architecture -- Requirements Definition -- Sensor-Input Requirements -- Data-processing Requirements -- Control of Effectors -- Engine and Control Self-test -- Environmental Requirements -- Vehicle Interface -- Controller Architecture -- Function Allocation -- Failure Detection and Response -- Hardware Design Rules -- Postflight Data Analysis -- Software Requirements -- 7.5 References -- Chapter 8. Design of Propellant Tanks -- 8.1 Design Configurations -- Prepackaged Storable-Liquid Systems -- Booster-Stage Systems -- Upper-Stage Systems -- 8.2 Design Considerations -- Propellant Properties -- Shape and Size of Propellant Tank -- Propellant-Tank Arrangement -- Structural Loads -- Safety Factors -- Material and Fabrication Considerations -- Design Problem -- 8.3 Structural Design -- Spherical Tanks -- Ellipsoidal and Spherical Ends (Fig. 8-6) -- Cylindrical Section -- Axial Compressive Loading on the Cylindrical Section -- Water-Hammer Effects Due to Impact -- 8.4 Storable-Liquid-Propellant Tank Design -- Tank-Material Compatibility -- Tank Construction -- Wall Surface Requirements -- 8.5 Cryogenic Liquid-Propellant Tank Design -- Insulation Requirements for Cryogenic-Propellant Tanks -- Basic Insulation Types -- Selection of Tank-Insulation Designs -- Insulation for Common Bulkheads -- 8.6 Composite Liquid-Propellant Tank Design -- 8.7 Design of Propellant-Tank Pressurant Diffusers -- 8.8 Propellant Expulsion Under Zero-Gravity or Oscillatory g-Loading Conditions -- Settling -- Propellant Management -- Metallic Diaphragms -- Elastomeric Diaphragms -- Bellows -- Pistons -- Surface-Tension Devices. Chapter 9. Design of Interconnecting Components and Mounts. |
| Record Nr. | UNINA-9910956007803321 |
|
Huzel Dieter K
|
||
| Washington, D.C., : American Institute of Aeronautics and Astronautics, 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||