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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 | ||
| ||
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 | ||
| ||
