Advanced control of aircraft, rockets, and spacecraft [[electronic resource] /] / Ashish Tewari |
Autore | Tewari Ashish |
Pubbl/distr/stampa | Hoboken, N.J., : Wiley, 2011 |
Descrizione fisica | 1 online resource (456 p.) |
Disciplina |
500
629.11 |
Collana | Aerospace Series |
Soggetto topico |
Flight control
Airplanes - Control systems Space vehicles - Control systems Rockets (Aeronautics) - Control systems |
ISBN |
1-119-97274-4
1-283-17775-7 9786613177759 1-119-97119-5 1-119-97120-9 |
Classificazione | TEC002000 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Advanced Control of Aircraft, Spacecraft and Rockets; Contents; Series Preface; Preface; 1 Introduction; 1.1 Notation and Basic Definitions; 1.2 Control Systems; 1.2.1 Linear Tracking Systems; 1.2.2 Linear Time-Invariant Tracking Systems; 1.3 Guidance and Control of Flight Vehicles; 1.4 Special Tracking Laws; 1.4.1 Proportional Navigation Guidance; 1.4.2 Cross-Product Steering; 1.4.3 Proportional-Integral-Derivative Control; 1.5 Digital Tracking System; 1.6 Summary; Exercises; References; 2 Optimal Control Techniques; 2.1 Introduction; 2.2 Multi-variable Optimization
2.3 Constrained Minimization2.3.1 Equality Constraints; 2.3.2 Inequality Constraints; 2.4 Optimal Control of Dynamic Systems; 2.4.1 Optimality Conditions; 2.5 The Hamiltonian and the Minimum Principle; 2.5.1 Hamilton-Jacobi-Bellman Equation; 2.5.2 Linear Time-Varying System with Quadratic Performance Index; 2.6 Optimal Control with End-Point State Equality Constraints; 2.6.1 Euler-Lagrange Equations; 2.6.2 Special Cases; 2.7 Numerical Solution of Two-Point Boundary Value Problems; 2.7.1 Shooting Method; 2.7.2 Collocation Method; 2.8 Optimal Terminal Control with Interior Time Constraints 2.8.1 Optimal Singular Control2.9 Tracking Control; 2.9.1 Neighboring Extremal Method and Linear Quadratic Control; 2.10 Stochastic Processes; 2.10.1 Stationary Random Processes; 2.10.2 Filtering of Random Noise; 2.11 Kalman Filter; 2.12 Robust Linear Time-Invariant Control; 2.12.1 LQG/LTR Method; 2.12.2 H2/H8 Design Methods; 2.13 Summary; Exercises; References; 3 Optimal Navigation and Control of Aircraft; 3.1 Aircraft Navigation Plant; 3.1.1 Wind Speed and Direction; 3.1.2 Navigational Subsystems; 3.2 Optimal Aircraft Navigation; 3.2.1 Optimal Navigation Formulation 3.2.2 Extremal Solution of the Boundary-Value Problem: Long-Range Flight Example3.2.3 Great Circle Navigation; 3.3 Aircraft Attitude Dynamics; 3.3.1 Translational and Rotational Kinetics; 3.3.2 Attitude Relative to the Velocity Vector; 3.4 Aerodynamic Forces and Moments; 3.5 Longitudinal Dynamics; 3.5.1 Longitudinal Dynamics Plant; 3.6 Optimal Multi-variable Longitudinal Control; 3.7 Multi-input Optimal Longitudinal Control; 3.8 Optimal Airspeed Control; 3.8.1 LQG/LTR Design Example; 3.8.2 H8 Design Example; 3.8.3 Altitude and Mach Control; 3.9 Lateral-Directional Control Systems 3.9.1 Lateral-Directional Plant3.9.2 Optimal Roll Control; 3.9.3 Multi-variable Lateral-Directional Control: Heading-Hold Autopilot; 3.10 Optimal Control of Inertia-Coupled Aircraft Rotation; 3.11 Summary; Exercises; References; 4 Optimal Guidance of Rockets; 4.1 Introduction; 4.2 Optimal Terminal Guidance of Interceptors; 4.3 Non-planar Optimal Tracking System for Interceptors: 3DPN; 4.4 Flight in a Vertical Plane; 4.5 Optimal Terminal Guidance; 4.6 Vertical Launch of a Rocket (Goddard's Problem); 4.7 Gravity-Turn Trajectory of Launch Vehicles 4.7.1 Launch to Circular Orbit: Modulated Acceleration |
Record Nr. | UNINA-9910139618703321 |
Tewari Ashish
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Hoboken, N.J., : Wiley, 2011 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced control of aircraft, rockets, and spacecraft / / Ashish Tewari |
Autore | Tewari Ashish |
Edizione | [1st ed.] |
Pubbl/distr/stampa | Hoboken, N.J., : Wiley, 2011 |
Descrizione fisica | 1 online resource (456 p.) |
Disciplina |
500
629.11 |
Collana | Aerospace Series |
Soggetto topico |
Flight control
Airplanes - Control systems Space vehicles - Control systems Rockets (Aeronautics) - Control systems |
ISBN |
1-119-97274-4
1-283-17775-7 9786613177759 1-119-97119-5 1-119-97120-9 |
Classificazione | TEC002000 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Advanced Control of Aircraft, Spacecraft and Rockets; Contents; Series Preface; Preface; 1 Introduction; 1.1 Notation and Basic Definitions; 1.2 Control Systems; 1.2.1 Linear Tracking Systems; 1.2.2 Linear Time-Invariant Tracking Systems; 1.3 Guidance and Control of Flight Vehicles; 1.4 Special Tracking Laws; 1.4.1 Proportional Navigation Guidance; 1.4.2 Cross-Product Steering; 1.4.3 Proportional-Integral-Derivative Control; 1.5 Digital Tracking System; 1.6 Summary; Exercises; References; 2 Optimal Control Techniques; 2.1 Introduction; 2.2 Multi-variable Optimization
2.3 Constrained Minimization2.3.1 Equality Constraints; 2.3.2 Inequality Constraints; 2.4 Optimal Control of Dynamic Systems; 2.4.1 Optimality Conditions; 2.5 The Hamiltonian and the Minimum Principle; 2.5.1 Hamilton-Jacobi-Bellman Equation; 2.5.2 Linear Time-Varying System with Quadratic Performance Index; 2.6 Optimal Control with End-Point State Equality Constraints; 2.6.1 Euler-Lagrange Equations; 2.6.2 Special Cases; 2.7 Numerical Solution of Two-Point Boundary Value Problems; 2.7.1 Shooting Method; 2.7.2 Collocation Method; 2.8 Optimal Terminal Control with Interior Time Constraints 2.8.1 Optimal Singular Control2.9 Tracking Control; 2.9.1 Neighboring Extremal Method and Linear Quadratic Control; 2.10 Stochastic Processes; 2.10.1 Stationary Random Processes; 2.10.2 Filtering of Random Noise; 2.11 Kalman Filter; 2.12 Robust Linear Time-Invariant Control; 2.12.1 LQG/LTR Method; 2.12.2 H2/H8 Design Methods; 2.13 Summary; Exercises; References; 3 Optimal Navigation and Control of Aircraft; 3.1 Aircraft Navigation Plant; 3.1.1 Wind Speed and Direction; 3.1.2 Navigational Subsystems; 3.2 Optimal Aircraft Navigation; 3.2.1 Optimal Navigation Formulation 3.2.2 Extremal Solution of the Boundary-Value Problem: Long-Range Flight Example3.2.3 Great Circle Navigation; 3.3 Aircraft Attitude Dynamics; 3.3.1 Translational and Rotational Kinetics; 3.3.2 Attitude Relative to the Velocity Vector; 3.4 Aerodynamic Forces and Moments; 3.5 Longitudinal Dynamics; 3.5.1 Longitudinal Dynamics Plant; 3.6 Optimal Multi-variable Longitudinal Control; 3.7 Multi-input Optimal Longitudinal Control; 3.8 Optimal Airspeed Control; 3.8.1 LQG/LTR Design Example; 3.8.2 H8 Design Example; 3.8.3 Altitude and Mach Control; 3.9 Lateral-Directional Control Systems 3.9.1 Lateral-Directional Plant3.9.2 Optimal Roll Control; 3.9.3 Multi-variable Lateral-Directional Control: Heading-Hold Autopilot; 3.10 Optimal Control of Inertia-Coupled Aircraft Rotation; 3.11 Summary; Exercises; References; 4 Optimal Guidance of Rockets; 4.1 Introduction; 4.2 Optimal Terminal Guidance of Interceptors; 4.3 Non-planar Optimal Tracking System for Interceptors: 3DPN; 4.4 Flight in a Vertical Plane; 4.5 Optimal Terminal Guidance; 4.6 Vertical Launch of a Rocket (Goddard's Problem); 4.7 Gravity-Turn Trajectory of Launch Vehicles 4.7.1 Launch to Circular Orbit: Modulated Acceleration |
Record Nr. | UNINA-9910818323903321 |
Tewari Ashish
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Hoboken, N.J., : Wiley, 2011 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aircraft engineering and aerospace technology |
Pubbl/distr/stampa | Bradford, England : , : Emerald Group Pub. |
Descrizione fisica | 1 online resource |
Disciplina | 629.11 |
Soggetto topico |
Aeronautics - Systems engineering
Astronautics - Systems engineering Airplanes - Equipment and supplies Space vehicles - Equipment and supplies Aerospace industries |
Soggetto genere / forma |
Periodicals.
Electronic journals. |
ISSN | 1758-4213 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Periodico |
Lingua di pubblicazione | eng |
Record Nr. | UNISA-996357748603316 |
Bradford, England : , : Emerald Group Pub. | ||
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Lo trovi qui: Univ. di Salerno | ||
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Aircraft engineering and aerospace technology |
Pubbl/distr/stampa | Bradford, England : , : Emerald Group Pub. |
Descrizione fisica | 1 online resource |
Disciplina | 629.11 |
Soggetto topico |
Aeronautics - Systems engineering
Astronautics - Systems engineering Airplanes - Equipment and supplies Space vehicles - Equipment and supplies Aerospace industries |
Soggetto genere / forma | Periodicals. |
ISSN | 1758-4213 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Periodico |
Lingua di pubblicazione | eng |
Record Nr. | UNISA-996398346003316 |
Bradford, England : , : Emerald Group Pub. | ||
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Lo trovi qui: Univ. di Salerno | ||
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Aircraft engineering and aerospace technology |
Pubbl/distr/stampa | Bradford, England : , : Emerald Group Pub. |
Descrizione fisica | 1 online resource |
Disciplina | 629.11 |
Soggetto topico |
Aeronautics - Systems engineering
Astronautics - Systems engineering Airplanes - Equipment and supplies Space vehicles - Equipment and supplies Aerospace industries |
Soggetto genere / forma | Periodicals. |
ISSN | 1758-4213 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Periodico |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910143344203321 |
Bradford, England : , : Emerald Group Pub. | ||
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Lo trovi qui: Univ. Federico II | ||
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Beamed-Mobility Engineering : Wireless-Power Beaming to Aircrafts, Spacecrafts and Rockets |
Autore | Mori Koichi |
Edizione | [1st ed.] |
Pubbl/distr/stampa | Singapore : , : Springer, , 2024 |
Descrizione fisica | 1 online resource (260 pages) |
Disciplina | 629.11 |
Altri autori (Persone) |
OdaYasuhisa
MasayukiTakahashi ShimamuraKohei |
Collana | Springer Tracts in Electrical and Electronics Engineering Series |
ISBN | 981-9946-18-2 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Intro -- Foreword -- Preface -- Contents -- Chapter 1: Wireless Power Transfer Via Microwave for Mobilities -- Introduction -- Review of Microwave Power Transmission to UAVs -- Receiver Systems -- Principle of Rectifier -- High-Frequency Rectifiers (Millimeter Wave) -- Methods of Operating Diodes at High Frequencies -- S and B Band Rectifier Circuits -- Dual-Band Rectifiers -- High-Power Operation Rectifiers -- Tube-Type Rectifier -- Wireless Power Transfer vs. Battery -- Feasibility of Microwave Powered Flight of UAVs -- Beam Collecting Efficiency ηbeam -- Beam Capture Efficiency on Rectenna ηcap -- Antenna Transmission Efficiency ηtra and RF-DC Conversion Efficiency ηRF - DC -- Operation Frequency Dependency: 5.8 GHz vs. 28 GHz -- Flight Demonstration of Microwave Power Transmission with Drone -- Mobilities Design -- Flight Demonstration -- References -- Chapter 2: Microwave Rocket -- What Is a Microwave Rocket? -- Thrust Generation Mechanism of Microwave Rocket -- Thrust Generation Experiment and Performance Trend of Microwave Rocket -- Experimental Application of High-Power Microwave Sources -- Thrust Measurement Experiment and Performance with a Single Pulse -- Millimeter-Wave Plasma in the Thruster -- Multi-Pulse Thrust Generation Experiment and Performance -- Impact on Beam Profile and Frequency -- Demonstration of Microwave Rocket -- Flight Experiment with a Single Pulse -- Flight Experiment with Multi-Pulse Operation -- Thrust Generation Experiment of Long-Distance Transmission Type Thruster with Beam Optical Conversion -- Microwave Rocket System Analysis -- Launch System Beam Source -- References -- Chapter 3: Laser Propulsion and Demonstrations -- Pulsed Laser Orbital Launcher -- Introduction -- What Is Pulsed Laser Propulsion? -- Propulsion Principle of the Pulsed Laser Propulsion System.
Various Vehicle Types and Their Research Trends -- Past Studies of Pulsed Laser Launch Systems -- Feasibility of Mass Space Transportation by Laser Propulsion -- Transportation to GEO Via Light Highway -- Flight Trajectory and Payload Ratio -- Cost Evaluation -- Consideration of Laser Types and Necessary Innovations -- Summary -- Demonstration of Laser Propulsion and Space Debris Removal (Demonstration Movie Available) -- Launch Demonstration of Laser-Driven In-Tube Accelerator (LITA) with Gas Driver -- Launch Demonstration of Wall-Ablative, Laser-Driven In-Tube Accelerator -- Demonstration of Satellite Spin Breaking Using a TEA CO2 Laser (2016) -- Demonstration of Satellite Spin Breaking Using an Nd: YLF Laser (2021) -- References -- Chapter 4: Spectroscopy of Air Discharge Plasmas Induced by a Gyrotron Beam -- Introduction -- Optical Emission Spectroscopy (OES) -- Benefits of OES for the Measurement of Millimeter-Wave Discharges -- General Remarks on Optical Radiation of Atoms and Molecules -- Measurement of Electron Number Density -- Fundamentals of Spectrum Broadening -- Stark Broadening -- Instrumental Broadening -- Natural Broadening -- Doppler Broadening -- Pressure Broadening (Van der Waals Broadening) -- Practical Use of Stark Broadening in Millimeter-Wave or Microwave Discharge Plasmas -- Measurement of Electrons and Gas Temperature -- Fundamentals of Emission Spectra of Air Discharge Plasmas -- Theoretical Scheme for Calculating Molecular Band Spectrum -- Practical Use of Molecular Band Spectrum Analysis for the Temperature Measurement in Air Discharge Plasmas -- Density and Temperature Measurements in Other Ambient Gases -- References -- Chapter 5: Experimental Studies of Microwave Discharge Induced by Gyrotron -- Introduction -- Ionization Threshold Models -- Microwave Discharge in the Over-Critical Condition. Microwave Discharge in the Under-Critical Condition -- Summary -- References -- Chapter 6: Modeling and Theoretical Studies on Beamed-Induced Plasma -- Introduction to Theoretical Studies -- Fluid Modeling for Overcritical Millimeter-Wave Discharge -- Particle Modeling for Overcritical Millimeter-Wave Discharge -- Past Simulations by PIC-MCC Model -- Modeling for Subcritical Discharge -- Numerical Analysis of ``Comb-Shaped´´ Structures -- Numerical Reproduction and Structure Forming Mechanism -- Effect of the Structure on Ionization-Front Propagation -- One-Dimensional Consideration of Ionization-Front Propagation in Under-Critical Condition -- Ionization-Front Propagation with Excited Neutral Particles Carried via Photons -- Transportation of Exited Neutral Particles via Photons -- Diffusion Approximation of Transportation of Electronically Excited Particle via Photons -- One-Dimensional Model with Simple Assumption -- One-Dimensional Computation -- References -- Chapter 7: Laser-Supported Detonation -- Numerical Analyses of Laser-Supported Detonation Wave in Air -- Introduction -- Computational Model and Method -- Computational Condition -- Results and Discussion -- Results of the Standard Atmosphere of pa = 1 atm -- Results of the Reduced-Pressure Atmosphere -- Comparison of the Wave Speeds -- Summary -- Experimental Studies of Laser-Supported Detonation -- Propagation Velocity of Laser-Supported Detonation Wave -- Termination Conditions of LSD Wave -- Energy Conversion Efficiency in LSD -- Summary -- References -- Chapter 8: High-Power Beam Source and Beam Transmission -- Introduction of Electromagnetism -- Features of the Gaussian Beam -- Relationship Between Beam Diameter and Frequency -- Frequency of Electromagnetic Waves and Power Source -- Oscillation Caused by Electric Circuit -- Microwave Electron Tube -- Magnetron -- Klystron -- Gyrotron. Synchrotron Radiation -- Free-Electron Laser -- Technology for High-Power Beam Source -- Beam Source: Gyrotron Tube -- High-Voltage Power Supply for Gyrotron -- Superconducting Magnet -- Matching Optical Unit -- Auxiliaries -- Technology for High-Power Beam Transmission -- Waveguide -- Miter Bend -- Dummy Load -- Power Selection and Control Equipment -- Example of High-Power Beam Source -- Electronic Cyclotron Heating System for Fusion Plasma -- References -- Chapter 9: Retrodirective Wireless Optical Energy Transmission Using Optical Phase Conjugation -- Atmospheric Disturbance -- Turbulence-Induced Beam Spreading and Beam Wandering -- Wireless Optical Power Transfer Technologies -- Gimbal Tracking -- Adaptive Optics -- Optical Phase Conjugation -- Principles of Optical Phase Conjugation -- Phase-Conjugate Light Generation Technique -- Nonlinear Optical Element -- Digital Phase Conjugation -- References -- Chapter 10: Diode Laser-Sustained Plasma for Continuous-Wave Laser Propulsion -- Introduction -- LSP -- Background of LSP -- Principle of Laser Absorption Process -- Experimental Apparatus -- Results and Discussion -- LSP Generation -- Fluctuation of LSP -- Temperature Measurement -- Fractional Absorption and Radiation Loss -- Conclusion -- References. |
Record Nr. | UNINA-9910855390603321 |
Mori Koichi
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Singapore : , : Springer, , 2024 | ||
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Lo trovi qui: Univ. Federico II | ||
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Fault diagnosis and fault-tolerant control and guidance for aerospace vehicles : from theory to application / / Ali Zolghadri [and four others] |
Autore | Zolghadri Ali |
Edizione | [1st ed. 2014.] |
Pubbl/distr/stampa | London : , : Springer, , 2014 |
Descrizione fisica | 1 online resource (xvi, 216 pages) : illustrations (some color) |
Disciplina |
629.11
629.8 |
Collana | Advances in Industrial Control |
Soggetto topico |
Airplanes - Control systems
Fault tolerance (Engineering) |
ISBN | 1-4471-5313-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Basic Concepts: Academic State of the Art and Industrial State of Practice -- Robust Fault Detection in Aircraft Control Surface Servo-Loop: Oscillatory Failure Case -- Robust Fault Detection in Aircraft Control Surface Servo-Loop: Runaway and Jamming -- Non-conservative H-infinity/H2 FDD Design: LTI Case -- H-infinity/H2 FDD Design for LPV Case -- An Active Fault-tolerant Flight Control Strategy -- Final Remarks. |
Record Nr. | UNINA-9910299760203321 |
Zolghadri Ali
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London : , : Springer, , 2014 | ||
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Lo trovi qui: Univ. Federico II | ||
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Journal of thermophysics and heat transfer |
Pubbl/distr/stampa | Washington, : American Institute of Aeronautics and Astronautics |
Disciplina | 629.11 |
ISSN | 0887-8722 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Periodico |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990008995640403321 |
Washington, : American Institute of Aeronautics and Astronautics | ||
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Lo trovi qui: Univ. Federico II | ||
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Space engineering : proceedings of the Second international conference on space engineering : held at the FondazioneGiorgio Cini, Isola di San Giorgio, Venice, Italy, May 7-10, 1969 / edited by G.A. Partel |
Autore | SPACE ENGINEERING, 2., 1969, Venezia |
Pubbl/distr/stampa | Dordrecht : D. Reidel, copyr. 1970 |
Descrizione fisica | XI, 728 p. : ill. ; 24 cm |
Disciplina | 629.11 |
Collana | Astrophysics and space science library |
Soggetto non controllato | Volo spaziale |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ita |
Record Nr. | UNINA-990000056670403321 |
SPACE ENGINEERING, 2., 1969, Venezia
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Dordrecht : D. Reidel, copyr. 1970 | ||
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Lo trovi qui: Univ. Federico II | ||
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Theory of aerospace propulsion / / Pasquale M. Sforza |
Autore | Sforza P. M |
Edizione | [1st ed.] |
Pubbl/distr/stampa | Waltham, Mass., : Academic Press, c2012 |
Descrizione fisica | 1 online resource (703 p.) |
Disciplina |
629.1/1
629.11 |
Collana | Aerospace Engineering |
Soggetto topico | Jet propulsion |
ISBN |
1-283-29364-1
9786613293640 0-12-384889-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Front Cover; Theory of Aerospace Propulsion; Copyright; Contents; Preface; Chapter 1 - Idealized Flow Machines; 1.1 Conservation Equations; 1.2 Flow Machines with No Heat Addition: The Propeller; 1.3 Flow Machines with P = 0 and Q = Constant: The Turbojet, Ramjet, and Scramjet; 1.4 Flow Machines with P = 0, Q = Constant, and A0 = 0: The Rocket; 1.5 The Special Case of Combined Heat and Power: The Turbofan; 1.6 Force Field for Air-Breathing Engines; 1.7 Conditions for Maximum Thrust; 1.8 Example: Jet and Rocket Engine Performance; 1.9 Nomenclature; Reference
Chapter 2 - Quasi-One-Dimensional Flow Equations2.1 Introduction; 2.2 Equation of State; 2.3 Speed of Sound; 2.4 Mach Number; 2.5 Conservation of Mass; 2.6 Conservation of Energy; 2.7 Example: Heating Values for Different Fuel-Oxidizer Combinations; 2.8 Conservation of Species; 2.9 Conservation of Momentum; 2.10 Impulse Function; 2.11 Stagnation Pressure; 2.12 Equations of Motion in Standard Form; 2.13 Example: Flow in a Duct with Friction; 2.14 Nomenclature; References; Chapter 3 - Idealized Cycle Analysis of Jet Propulsion Engines; 3.1 Introduction; 3.2 General Jet Engine Cycle 3.3 Ideal Jet Engine Cycle Analysis3.4 Ideal Turbojet in Maximum Power Take-Off; 3.5 Ideal Turbojet in High Subsonic Cruise in The Stratosphere; 3.6 Ideal Turbojet in Supersonic Cruise in The Stratosphere; 3.7 Ideal Ramjet in High Supersonic Cruise in The Stratosphere; 3.8 Ideal Turbofan in Maximum Power Take-Off; 3.9 Ideal Turbofan in High Subsonic Cruise in The Stratosphere; 3.10 Ideal Internal Turbofan in Supersonic Cruise in The Stratosphere; 3.11 Real Engine Operations; 3.12 Nomenclature; 3.13 Exercises; References; Chapter 4 - Combustion Chambers for Air-Breathing Engines 4.1 Combustion Chamber Attributes4.2 Modeling the Chemical Energy Release; 4.3 Constant Area Combustors; 4.4 Example: Constant Area Combustor; 4.5 Constant Pressure Combustors; 4.6 Fuels for Air-Breathing Engines; 4.7 Combustor Efficiency; 4.8 Combustor Configuration; 4.9 Example: Secondary Air for Cooling; 4.10 Criteria for Equilibrium in Chemical Reactions; 4.11 Calculation of Equilibrium Compositions; 4.12 Example: Homogeneous Reactions with a Direct Solution; 4.13 Example: Homogeneous Reactions with Trial-And-Error Solution 4.14 Example: Estimation of Importance of Neglected Product Species4.15 Adiabatic Flame Temperature; 4.16 Example: Adiabatic Flame Temperature for Stoichiometric H2-O2 Mixture; 4.17 Nomenclature; References; Chapter 5 - Nozzles; 5.1 Nozzle Characteristics and Simplifying Assumptions; 5.2 Flow in a Nozzle with Simple Area Change; 5.3 Mass Flow in an Isentropic Nozzle; 5.4 Nozzle Operation; 5.5 Normal Shock inside the Nozzle; 5.6 Example: Shock in Nozzle; 5.7 Two-Dimensional Considerations in Nozzle Flows; 5.8 Example: Overexpanded Nozzles; 5.9 Example: Underexpanded Nozzles 5.10 Afterburning for Increased Thrust |
Record Nr. | UNINA-9910817660603321 |
Sforza P. M
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Waltham, Mass., : Academic Press, c2012 | ||
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Lo trovi qui: Univ. Federico II | ||
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