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MARC Lista (tabellare)
Advanced aircraft design : conceptual design, analysis and optimization of subsonic civil airplanes / / Egbert Torenbeek.(Delft University of Technology, The Netherlands)
Advanced aircraft design : conceptual design, analysis and optimization of subsonic civil airplanes / / Egbert Torenbeek.(Delft University of Technology, The Netherlands)
Autore Torenbeek Egbert
Pubbl/distr/stampa Chichester, West Sussex, U.K. : , : Wiley, , [2013]
Descrizione fisica 1 online resource (438 p.)
Disciplina 629.133/34
Collana Aerospace series
THEi Wiley ebooks
Soggetto topico Avions de transport - Disseny i construcció
Avions de reacció - Disseny i construcció
Transport planes - Design and construction
Jet planes - Design and construction
Airplanes - Performance
ISBN 1-118-56809-5
1-118-56810-9
1-118-56808-7
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ADVANCED AIRCRAFT DESIGN; Contents; Foreword; Series Preface; Preface; Acknowledgements; 1 Design of the Well-Tempered Aircraft; 1.1 How Aircraft Design Developed; 1.1.1 Evolution of Jetliners and Executive Aircraft; 1.1.2 A Framework for Advanced Design; 1.1.3 Analytical Design Optimization; 1.1.4 Computational Design Environment; 1.2 Concept Finding; 1.2.1 Advanced Design; 1.2.2 Pre-conceptual Studies; 1.3 Product Development; 1.3.1 Concept Definition; 1.3.2 Preliminary Design; 1.3.3 Detail Design; 1.4 Baseline Design in a Nutshell; 1.4.1 Baseline Sizing; 1.4.2 Power Plant
1.4.3 Weight and Balance 1.4.4 Structure; 1.4.5 Performance Analysis; 1.4.6 Closing the Loop; 1.5 Automated Design Synthesis; 1.5.1 Computational Systems Requirements; 1.5.2 Examples; 1.5.3 Parametric Surveys; 1.6 Technology Assessment; 1.7 Structure of the Optimization Problem; 1.7.1 Analysis Versus Synthesis; 1.7.2 Problem Classification; Bibliography; 2 Early Conceptual Design; 2.1 Scenario and Requirements; 2.1.1 What Drives a Design?; 2.1.2 Civil Airplane Categories; 2.1.3 Top Level Requirements; 2.2 Weight Terminology and Prediction; 2.2.1 Method Classification
2.2.2 Basic Weight Components 2.2.3 Weight Limits; 2.2.4 Transport Capability; 2.3 The Unity Equation; 2.3.1 Mission Fuel; 2.3.2 Empty Weight; 2.3.3 Design Weights; 2.4 Range Parameter; 2.4.1 Aerodynamic Efficiency; 2.4.2 Specific Fuel Consumption and Overall Efficiency; 2.4.3 Best Cruise Speed; 2.5 Environmental Issues; 2.5.1 Energy and Payload Fuel Efficiency; 2.5.2 'Greener by Design'; Bibliography; 3 Propulsion and Engine Technology; 3.1 Propulsion Leading the Way; 3.2 Basic Concepts of Jet Propulsion; 3.2.1 Turbojet Thrust; 3.2.2 Turbofan Thrust; 3.2.3 Specific Fuel Consumption
3.2.4 Overall Efficiency 3.2.5 Thermal and Propulsive Efficiency; 3.2.6 Generalized Performance; 3.2.7 Mach Number and Altitude Effects; 3.3 Turboprop Engines; 3.3.1 Power and Specific Fuel Consumption; 3.3.2 Generalized Performance; 3.3.3 High Speed Propellers; 3.4 Turbofan Engine Layout; 3.4.1 Bypass Ratio Trends; 3.4.2 Rise and Fall of the Propfan; 3.4.3 Rebirth of the Open Rotor?; 3.5 Power Plant Selection; 3.5.1 Power Plant Location; 3.5.2 Alternative Fuels; 3.5.3 Aircraft Noise; Bibliography; 4 Aerodynamic Drag and Its Reduction; 4.1 Basic Concepts
4.1.1 Lift, Drag and Aerodynamic Efficiency 4.1.2 Drag Breakdown and Definitions; 4.2 Decomposition Schemes and Terminology; 4.2.1 Pressure and Friction Drag; 4.2.2 Viscous Drag; 4.2.3 Vortex Drag; 4.2.4 Wave Drag; 4.3 Subsonic Parasite and Induced Drag; 4.3.1 Parasite Drag; 4.3.2 Monoplane Induced Drag; 4.3.3 Biplane Induced Drag; 4.3.4 Multiplane and Boxplane Induced Drag; 4.4 Drag Polar Representations; 4.4.1 Two-term Approximation; 4.4.2 Three-term Approximation; 4.4.3 Reynolds Number Effects; 4.4.4 Compressibility Correction; 4.5 Drag Prediction; 4.5.1 Interference Drag
4.5.2 Roughness and Excrescences
Record Nr. UNINA-9910141604603321
Torenbeek Egbert  
Chichester, West Sussex, U.K. : , : Wiley, , [2013]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Advanced aircraft design : conceptual design, analysis and optimization of subsonic civil airplanes / / Egbert Torenbeek.(Delft University of Technology, The Netherlands)
Advanced aircraft design : conceptual design, analysis and optimization of subsonic civil airplanes / / Egbert Torenbeek.(Delft University of Technology, The Netherlands)
Autore Torenbeek Egbert
Edizione [1st ed.]
Pubbl/distr/stampa Chichester, West Sussex, U.K. : , : Wiley, , [2013]
Descrizione fisica 1 online resource (438 p.)
Disciplina 629.133/34
Collana Aerospace series
THEi Wiley ebooks
Soggetto topico Avions de transport - Disseny i construcció
Avions de reacció - Disseny i construcció
Transport planes - Design and construction
Jet planes - Design and construction
Airplanes - Performance
ISBN 1-118-56809-5
1-118-56810-9
1-118-56808-7
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ADVANCED AIRCRAFT DESIGN; Contents; Foreword; Series Preface; Preface; Acknowledgements; 1 Design of the Well-Tempered Aircraft; 1.1 How Aircraft Design Developed; 1.1.1 Evolution of Jetliners and Executive Aircraft; 1.1.2 A Framework for Advanced Design; 1.1.3 Analytical Design Optimization; 1.1.4 Computational Design Environment; 1.2 Concept Finding; 1.2.1 Advanced Design; 1.2.2 Pre-conceptual Studies; 1.3 Product Development; 1.3.1 Concept Definition; 1.3.2 Preliminary Design; 1.3.3 Detail Design; 1.4 Baseline Design in a Nutshell; 1.4.1 Baseline Sizing; 1.4.2 Power Plant
1.4.3 Weight and Balance 1.4.4 Structure; 1.4.5 Performance Analysis; 1.4.6 Closing the Loop; 1.5 Automated Design Synthesis; 1.5.1 Computational Systems Requirements; 1.5.2 Examples; 1.5.3 Parametric Surveys; 1.6 Technology Assessment; 1.7 Structure of the Optimization Problem; 1.7.1 Analysis Versus Synthesis; 1.7.2 Problem Classification; Bibliography; 2 Early Conceptual Design; 2.1 Scenario and Requirements; 2.1.1 What Drives a Design?; 2.1.2 Civil Airplane Categories; 2.1.3 Top Level Requirements; 2.2 Weight Terminology and Prediction; 2.2.1 Method Classification
2.2.2 Basic Weight Components 2.2.3 Weight Limits; 2.2.4 Transport Capability; 2.3 The Unity Equation; 2.3.1 Mission Fuel; 2.3.2 Empty Weight; 2.3.3 Design Weights; 2.4 Range Parameter; 2.4.1 Aerodynamic Efficiency; 2.4.2 Specific Fuel Consumption and Overall Efficiency; 2.4.3 Best Cruise Speed; 2.5 Environmental Issues; 2.5.1 Energy and Payload Fuel Efficiency; 2.5.2 'Greener by Design'; Bibliography; 3 Propulsion and Engine Technology; 3.1 Propulsion Leading the Way; 3.2 Basic Concepts of Jet Propulsion; 3.2.1 Turbojet Thrust; 3.2.2 Turbofan Thrust; 3.2.3 Specific Fuel Consumption
3.2.4 Overall Efficiency 3.2.5 Thermal and Propulsive Efficiency; 3.2.6 Generalized Performance; 3.2.7 Mach Number and Altitude Effects; 3.3 Turboprop Engines; 3.3.1 Power and Specific Fuel Consumption; 3.3.2 Generalized Performance; 3.3.3 High Speed Propellers; 3.4 Turbofan Engine Layout; 3.4.1 Bypass Ratio Trends; 3.4.2 Rise and Fall of the Propfan; 3.4.3 Rebirth of the Open Rotor?; 3.5 Power Plant Selection; 3.5.1 Power Plant Location; 3.5.2 Alternative Fuels; 3.5.3 Aircraft Noise; Bibliography; 4 Aerodynamic Drag and Its Reduction; 4.1 Basic Concepts
4.1.1 Lift, Drag and Aerodynamic Efficiency 4.1.2 Drag Breakdown and Definitions; 4.2 Decomposition Schemes and Terminology; 4.2.1 Pressure and Friction Drag; 4.2.2 Viscous Drag; 4.2.3 Vortex Drag; 4.2.4 Wave Drag; 4.3 Subsonic Parasite and Induced Drag; 4.3.1 Parasite Drag; 4.3.2 Monoplane Induced Drag; 4.3.3 Biplane Induced Drag; 4.3.4 Multiplane and Boxplane Induced Drag; 4.4 Drag Polar Representations; 4.4.1 Two-term Approximation; 4.4.2 Three-term Approximation; 4.4.3 Reynolds Number Effects; 4.4.4 Compressibility Correction; 4.5 Drag Prediction; 4.5.1 Interference Drag
4.5.2 Roughness and Excrescences
Record Nr. UNINA-9910813177203321
Torenbeek Egbert  
Chichester, West Sussex, U.K. : , : Wiley, , [2013]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Advanced Aircraft Flight Performance : Including Environmental Performance / / Antonio Filippone
Advanced Aircraft Flight Performance : Including Environmental Performance / / Antonio Filippone
Autore Filippone Antonio <1965->
Edizione [Second edition.]
Pubbl/distr/stampa Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2022]
Descrizione fisica 1 online resource (831 pages)
Disciplina 629.132
Soggetto topico Airplanes - Performance
Airplanes - Design and construction
ISBN 9781624106408
9781624106392
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910780744203321
Filippone Antonio <1965->  
Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2022]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Advanced Aircraft Flight Performance : Including Environmental Performance / / Antonio Filippone
Advanced Aircraft Flight Performance : Including Environmental Performance / / Antonio Filippone
Autore Filippone Antonio <1965->
Edizione [Second edition.]
Pubbl/distr/stampa Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2022]
Descrizione fisica 1 online resource (831 pages)
Disciplina 629.132
Soggetto topico Airplanes - Performance
Airplanes - Design and construction
ISBN 9781624106408
9781624106392
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910809385003321
Filippone Antonio <1965->  
Reston, Virginia : , : American Institute of Aeronautics and Astronautics, Inc., , [2022]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh
Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh
Autore Dusenbury Mark
Edizione [Second edition.]
Pubbl/distr/stampa Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016
Descrizione fisica 1 online resource (ix, 230 pages)
Disciplina 629.1323
Soggetto topico Aerodynamics
Airplanes - Piloting
Airplanes - Performance
Soggetto genere / forma Electronic books.
ISBN 1-61954-334-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910467759703321
Dusenbury Mark  
Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh
Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh
Autore Dusenbury Mark
Edizione [Second edition.]
Pubbl/distr/stampa Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016
Descrizione fisica 1 online resource (ix, 230 pages)
Disciplina 629.1323
Soggetto topico Aerodynamics
Airplanes - Piloting
Airplanes - Performance
ISBN 1-61954-334-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910793325603321
Dusenbury Mark  
Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh
Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh
Autore Dusenbury Mark
Edizione [Second edition.]
Pubbl/distr/stampa Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016
Descrizione fisica 1 online resource (ix, 230 pages)
Disciplina 629.1323
Soggetto topico Aerodynamics
Airplanes - Piloting
Airplanes - Performance
ISBN 1-61954-334-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910817569703321
Dusenbury Mark  
Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
Autore Durham Wayne <1941->
Pubbl/distr/stampa Chichester, West Sussex, : John Wiley & Sons, Inc., 2013
Descrizione fisica 1 online resource (308 p.)
Disciplina 629.132/3
Collana Aerospace series
Soggetto topico Aerodynamics
Flight
Flight control
Airplanes - Performance
Soggetto genere / forma Electronic books.
ISBN 1-118-64680-0
1-118-64679-7
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover; Title Page; Copyright; Contents; Series Preface; Glossary; Chapter 1 Introduction; 1.1 Background; 1.2 Overview; 1.3 Customs and Conventions; References; Chapter 2 Coordinate Systems; 2.1 Background; 2.2 The Coordinate Systems; 2.2.1 The inertial reference frame, FI; 2.2.2 The earth-centered reference frame, FEC; 2.2.3 The earth-fixed reference frame, FE; 2.2.4 The local-horizontal reference frame, FH; 2.2.5 Body-fixed reference frames, FB; 2.2.6 Wind-axis system, FW; 2.2.7 Atmospheric reference frame; 2.3 Vector Notation; 2.4 Customs and Conventions; 2.4.1 Latitude and longitude
2.4.2 Body axes2.4.3 `The' body-axis system; 2.4.4 Aerodynamic angles; Problems; References; Chapter 3 Coordinate System Transformations; 3.1 Problem Statement; 3.2 Transformations; 3.2.1 Definitions; 3.2.2 Direction cosines; 3.2.3 Euler angles; 3.2.4 Euler parameters; 3.3 Transformations of Systems of Equations; 3.4 Customs and Conventions; 3.4.1 Names of Euler angles; 3.4.2 Principal values of Euler angles; Problems; Reference; Chapter 4 Rotating Coordinate Systems; 4.1 General; 4.2 Direction Cosines; 4.3 Euler Angles; 4.4 Euler Parameters; 4.5 Customs and Conventions
4.5.1 Angular velocity componentsProblems; Chapter 5 Inertial Accelerations; 5.1 General; 5.2 Inertial Acceleration of a Point; 5.2.1 Arbitrary moving reference frame; 5.2.2 Earth-centered moving reference frame; 5.2.3 Earth-fixed moving reference frame; 5.3 Inertial Acceleration of a Mass; 5.3.1 Linear acceleration; 5.3.2 Rotational acceleration; 5.4 States; 5.5 Customs and Conventions; 5.5.1 Linear velocity components; 5.5.2 Angular velocity components; 5.5.3 Forces; 5.5.4 Moments; 5.5.5 Groupings; Problems; Chapter 6 Forces and Moments; 6.1 General; 6.1.1 Assumptions; 6.1.2 State variables
6.1.3 State rates6.1.4 Flight controls; 6.1.5 Independent variables; 6.2 Non-Dimensionalization; 6.3 Non-Dimensional Coefficient Dependencies; 6.3.1 General; 6.3.2 Altitude dependencies; 6.3.3 Velocity dependencies; 6.3.4 Angle-of-attack dependencies; 6.3.5 Sideslip dependencies; 6.3.6 Angular velocity dependencies; 6.3.7 Control dependencies; 6.3.8 Summary of dependencies; 6.4 The Linear Assumption; 6.5 Tabular Data; 6.6 Customs and Conventions; Problems; Chapter 7 Equations of Motion; 7.1 General; 7.2 Body-Axis Equations; 7.2.1 Body-axis force equations; 7.2.2 Body-axis moment equations
7.2.3 Body-axis orientation equations (kinematic equations)7.2.4 Body-axis navigation equations; 7.3 Wind-Axis Equations; 7.3.1 Wind-axis force equations; 7.3.2 Wind-axis orientation equations (kinematic equations); 7.3.3 Wind-axis navigation equations; 7.4 Steady-State Solutions; 7.4.1 General; 7.4.2 Special cases; 7.4.3 The trim problem; Problems; Reference; Chapter 8 Linearization; 8.1 General; 8.2 Taylor Series; 8.3 Nonlinear Ordinary Differential Equations; 8.4 Systems of Equations; 8.5 Examples; 8.5.1 General; 8.5.2 A kinematic equation; 8.5.3 A moment equation; 8.5.4 A force equation
8.6 Customs and Conventions
Record Nr. UNINA-9910463787503321
Durham Wayne <1941->  
Chichester, West Sussex, : John Wiley & Sons, Inc., 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
Autore Durham Wayne <1941->
Pubbl/distr/stampa Chichester, West Sussex, : John Wiley & Sons, Inc., 2013
Descrizione fisica xix, 286 p. : ill
Disciplina 629.132/3
Collana Aerospace series
Soggetto topico Aerodynamics
Airplanes - Performance
Flight control
Flight
ISBN 9781118646793
1118646797
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910796091203321
Durham Wayne <1941->  
Chichester, West Sussex, : John Wiley & Sons, Inc., 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
Autore Durham Wayne <1941->
Edizione [1st ed.]
Pubbl/distr/stampa Chichester, West Sussex, : John Wiley & Sons, Inc., 2013
Descrizione fisica xix, 286 p. : ill
Disciplina 629.132/3
Collana Aerospace series
Soggetto topico Aerodynamics
Airplanes - Performance
Flight control
Flight
ISBN 9781118646793
1118646797
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover -- Title Page -- Copyright -- Contents -- Series Preface -- Glossary -- Chapter 1 Introduction -- 1.1 Background -- 1.2 Overview -- 1.3 Customs and Conventions -- References -- Chapter 2 Coordinate Systems -- 2.1 Background -- 2.2 The Coordinate Systems -- 2.2.1 The inertial reference frame, FI -- 2.2.2 The earth-centered reference frame, FEC -- 2.2.3 The earth-fixed reference frame, FE -- 2.2.4 The local-horizontal reference frame, FH -- 2.2.5 Body-fixed reference frames, FB -- 2.2.6 Wind-axis system, FW -- 2.2.7 Atmospheric reference frame -- 2.3 Vector Notation -- 2.4 Customs and Conventions -- 2.4.1 Latitude and longitude -- 2.4.2 Body axes -- 2.4.3 `The' body-axis system -- 2.4.4 Aerodynamic angles -- Problems -- References -- Chapter 3 Coordinate System Transformations -- 3.1 Problem Statement -- 3.2 Transformations -- 3.2.1 Definitions -- 3.2.2 Direction cosines -- 3.2.3 Euler angles -- 3.2.4 Euler parameters -- 3.3 Transformations of Systems of Equations -- 3.4 Customs and Conventions -- 3.4.1 Names of Euler angles -- 3.4.2 Principal values of Euler angles -- Problems -- Reference -- Chapter 4 Rotating Coordinate Systems -- 4.1 General -- 4.2 Direction Cosines -- 4.3 Euler Angles -- 4.4 Euler Parameters -- 4.5 Customs and Conventions -- 4.5.1 Angular velocity components -- Problems -- Chapter 5 Inertial Accelerations -- 5.1 General -- 5.2 Inertial Acceleration of a Point -- 5.2.1 Arbitrary moving reference frame -- 5.2.2 Earth-centered moving reference frame -- 5.2.3 Earth-fixed moving reference frame -- 5.3 Inertial Acceleration of a Mass -- 5.3.1 Linear acceleration -- 5.3.2 Rotational acceleration -- 5.4 States -- 5.5 Customs and Conventions -- 5.5.1 Linear velocity components -- 5.5.2 Angular velocity components -- 5.5.3 Forces -- 5.5.4 Moments -- 5.5.5 Groupings -- Problems -- Chapter 6 Forces and Moments -- 6.1 General.
6.1.1 Assumptions -- 6.1.2 State variables -- 6.1.3 State rates -- 6.1.4 Flight controls -- 6.1.5 Independent variables -- 6.2 Non-Dimensionalization -- 6.3 Non-Dimensional Coefficient Dependencies -- 6.3.1 General -- 6.3.2 Altitude dependencies -- 6.3.3 Velocity dependencies -- 6.3.4 Angle-of-attack dependencies -- 6.3.5 Sideslip dependencies -- 6.3.6 Angular velocity dependencies -- 6.3.7 Control dependencies -- 6.3.8 Summary of dependencies -- 6.4 The Linear Assumption -- 6.5 Tabular Data -- 6.6 Customs and Conventions -- Problems -- Chapter 7 Equations of Motion -- 7.1 General -- 7.2 Body-Axis Equations -- 7.2.1 Body-axis force equations -- 7.2.2 Body-axis moment equations -- 7.2.3 Body-axis orientation equations (kinematic equations) -- 7.2.4 Body-axis navigation equations -- 7.3 Wind-Axis Equations -- 7.3.1 Wind-axis force equations -- 7.3.2 Wind-axis orientation equations (kinematic equations) -- 7.3.3 Wind-axis navigation equations -- 7.4 Steady-State Solutions -- 7.4.1 General -- 7.4.2 Special cases -- 7.4.3 The trim problem -- Problems -- Reference -- Chapter 8 Linearization -- 8.1 General -- 8.2 Taylor Series -- 8.3 Nonlinear Ordinary Differential Equations -- 8.4 Systems of Equations -- 8.5 Examples -- 8.5.1 General -- 8.5.2 A kinematic equation -- 8.5.3 A moment equation -- 8.5.4 A force equation -- 8.6 Customs and Conventions -- 8.6.1 Omission of -- 8.6.2 Dimensional derivatives -- 8.6.3 Added mass -- 8.7 The Linear Equations -- 8.7.1 Linear equations -- 8.7.2 Matrix forms of the linear equations -- Problems -- References -- Chapter 9 Solutions to the Linear Equations -- 9.1 Scalar Equations -- 9.2 Matrix Equations -- 9.3 Initial Condition Response -- 9.3.1 Modal analysis -- 9.4 Mode Sensitivity and Approximations -- 9.4.1 Mode sensitivity -- 9.4.2 Approximations -- 9.5 Forced Response -- 9.5.1 Transfer functions.
9.5.2 Steady-state response -- Problems -- Chapter 10 Aircraft Flight Dynamics -- 10.1 Example: Longitudinal Dynamics -- 10.1.1 System matrices -- 10.1.2 State transition matrix and eigenvalues -- 10.1.3 Eigenvector analysis -- 10.1.4 Longitudinal mode sensitivity and approximations -- 10.1.5 Forced response -- 10.2 Example: Lateral-Directional Dynamics -- 10.2.1 System matrices -- 10.2.2 State transition matrix and eigenvalues -- 10.2.3 Eigenvector analysis -- 10.2.4 Lateral-directional mode sensitivity and approximations -- 10.2.5 Forced response -- Problems -- References -- Chapter 11 Flying Qualities -- 11.1 General -- 11.1.1 Method -- 11.1.2 Specifications and standards -- 11.2 MIL-F-8785C Requirements -- 11.2.1 General -- 11.2.2 Longitudinal flying qualities -- 11.2.3 Lateral-directional flying qualitities -- Problems -- References -- Chapter 12 Automatic Flight Control -- 12.1 Simple Feedback Systems -- 12.1.1 First-order systems -- 12.1.2 Second-order systems -- 12.1.3 A general representation -- 12.2 Example Feedback Control Applications -- 12.2.1 Roll mode -- 12.2.2 Short-period mode -- 12.2.3 Phugoid -- 12.2.4 Coupled roll-spiral oscillation -- Problems -- References -- Chapter 13 Trends in Automatic Flight Control -- 13.1 Overview -- 13.2 Dynamic Inversion -- 13.2.1 The controlled equations -- 13.2.2 The kinematic equations -- 13.2.3 The complementary equations -- 13.3 Control Allocation -- 13.3.1 Background -- 13.3.2 Problem statement -- 13.3.3 Optimality -- 13.3.4 Sub-optimal solutions -- 13.3.5 Optimal solutions -- 13.3.6 Near-optimal solutions -- Problems -- References -- Appendix A Example Aircraft -- Reference -- Appendix B Linearization -- B.1 Derivation of Frequently Used Derivatives -- B.2 Non-dimensionalization of the Rolling Moment Equation -- B.3 Body Axis Z-Force and Thrust Derivatives.
B.4 Non-dimensionalization of the Z-Force Equation -- Appendix C Derivation of Euler Parameters -- Appendix D Fedeeva's Algorithm -- Reference -- Appendix E MATLAB® Commands Used in the Text -- E.1 Using MATLAB® -- E.2 Eigenvalues and Eigenvectors -- E.3 State-Space Representation -- E.4 Transfer Function Representation -- E.5 Root Locus -- E.6 MATLAB® Functions (m-files) -- E.6.1 Example aircraft -- E.6.2 Mode sensitivity matrix -- E.6.3 Cut-and-try root locus gains -- E.7 Miscellaneous Applications and Notes -- E.7.1 Matrices -- E.7.2 Commands used to create Figures 10.2 and 10.3 -- Index.
Record Nr. UNINA-9910814647003321
Durham Wayne <1941->  
Chichester, West Sussex, : John Wiley & Sons, Inc., 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui