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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 |
9781118568095
1118568095 9781118568101 1118568109 9781118568088 1118568087 |
| 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 | ||
| ||
Aerodynamic design of transport aircraft [[electronic resource] /] / Ed Obert ; based on the original lecture series by Ed Obert amended by Ronald Slingerland
| Aerodynamic design of transport aircraft [[electronic resource] /] / Ed Obert ; based on the original lecture series by Ed Obert amended by Ronald Slingerland |
| Autore | Obert Ed |
| Pubbl/distr/stampa | Amsterdam, : Ios Press |
| Descrizione fisica | 1 online resource (656 p.) |
| Disciplina | 629.132/303 |
| Altri autori (Persone) | SlingerlandRonald |
| Soggetto topico |
Transport planes - Design and construction
Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-4416-1610-1
1-60750-407-3 600-00-1459-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Title page; Table of contents; Notations; Introduction; Pressure distributions; Airfoils; Swept wings; Low-speed aerodynamic limits; High-speed aerodynamic limits; Stability and control; Engine integration; Aircraft performance; Safety and regulations; Sources |
| Record Nr. | UNINA-9910454829003321 |
|
Obert Ed
|
||
| Amsterdam, : Ios Press | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerodynamic design of transport aircraft [[electronic resource] /] / Ed Obert ; based on the original lecture series by Ed Obert amended by Ronald Slingerland
| Aerodynamic design of transport aircraft [[electronic resource] /] / Ed Obert ; based on the original lecture series by Ed Obert amended by Ronald Slingerland |
| Autore | Obert Ed |
| Pubbl/distr/stampa | Amsterdam, : Ios Press |
| Descrizione fisica | 1 online resource (656 p.) |
| Disciplina | 629.132/303 |
| Altri autori (Persone) | SlingerlandRonald |
| Soggetto topico |
Transport planes - Design and construction
Aerodynamics |
| ISBN |
1-4416-1610-1
1-60750-407-3 600-00-1459-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Title page; Table of contents; Notations; Introduction; Pressure distributions; Airfoils; Swept wings; Low-speed aerodynamic limits; High-speed aerodynamic limits; Stability and control; Engine integration; Aircraft performance; Safety and regulations; Sources |
| Record Nr. | UNINA-9910777951603321 |
|
Obert Ed
|
||
| Amsterdam, : Ios Press | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Civil jet aircraft design / Lloyd R. Jenkinson, Paul Simkin, Darren Rhodes
| Civil jet aircraft design / Lloyd R. Jenkinson, Paul Simkin, Darren Rhodes |
| Autore | Jenkinson, Lloyd R. |
| Pubbl/distr/stampa | Reston, VA : American Insitute of Aeronautics and Astronautics, c1999 |
| Descrizione fisica | xi, 418 p. : ill. ; 25 cm |
| Disciplina | 629.1341 |
| Altri autori (Persone) |
Simpkin, Paul
Rhodes, Darren, 1972- |
| Collana | AIAA education series |
| Soggetto topico |
Jet planes - Design and construction
Transport planes - Design and construction |
| ISBN | 156347350X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991004139229707536 |
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Jenkinson, Lloyd R.
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| Reston, VA : American Insitute of Aeronautics and Astronautics, c1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration / / Lawrence E. Putnam
| Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration / / Lawrence E. Putnam |
| Autore | Putnam Lawrence E (Lawrence Elwood) |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (67 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aerodynamic characteristics
Transonic speed Wind tunnel tests Nacelles Transport aircraft Airplanes - Nacelles Transport planes - Design and construction Stability of airplanes, Longitudinal |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709713903321 |
|
Putnam Lawrence E (Lawrence Elwood)
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Methods for testing and evaluating cargo flooring for transport aircraft / / by M.P. Brokaw
| Methods for testing and evaluating cargo flooring for transport aircraft / / by M.P. Brokaw |
| Autore | Brokaw M. P. |
| Pubbl/distr/stampa | Madison, Wisconsin : , : United States Department of Agriculture, Forest Service, Forest Products Laboratory, , 1945 |
| Descrizione fisica | 1 online resource (70 unnumbered pages) : illustrations |
| Collana | Report |
| Soggetto topico |
Flooring - Testing
Transport planes - Design and construction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705299803321 |
|
Brokaw M. P.
|
||
| Madison, Wisconsin : , : United States Department of Agriculture, Forest Service, Forest Products Laboratory, , 1945 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax
| Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax |
| Autore | Lomax Ted L |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 |
| Descrizione fisica | 1 online resource (297 p.) |
| Disciplina | 629.134/31 |
| Collana | AIAA education series |
| Soggetto topico |
Airframes - Design and construction
Structural dynamics Transport planes - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-246-2
1-60086-118-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Nomenclature""; ""Chapter 1. Introduction""; ""1.1 Applicability of the Analysis""; ""1.2 Criteria""; ""1.3 Methodogy""; ""1.4 Static Aeroelastic Phenomena""; ""1.5 Sign Convention""; ""Chapter 2. Symmetrical Maneuvering Flight""; ""2.1 Symmetrical Maneuvering Flight Definition""; ""2.2 Symmetrical Maneuver Load Factors""; ""2.3 Steady-State Symmetrical Maneuvers""; ""2.4 Abrupt Pitching Maneuvers""; ""2.5 Abrupt Unchecked Pitch Maneuvers""; ""2.6 Abrupt Checked Maneuvers (Commercial Requirements)""
""2.7 Abrupt Checked Maneuvers (Military Requirements)""""2.8 Minimum Pitch Acceleration Requirements""; ""Chapter 3. Rolling Maneuvers""; ""3.1 Parameters Required for Structural Load Analyses""; ""3.2 Symmetrical Load Factors for Rolling Maneuvers""; ""3.3 Control Surface Deflections for Rolling Maneuvers""; ""3.4 Equations of Motion for Rolling Maneuvers""; ""3.5 Maximum Rolling Acceleration and Velocity Criteria""; ""3.6 Roll Termination Condition""; ""3.7 Nonlinear Lateral Control Inputs""; ""3.8 Aeroelastic Effects""; ""Chapter 4. Yawing Maneuvers"" ""4.1 Parameters Required for Structural Load Analyses""""4.2 Rudder Maneuver Requirements FAR 25 Criteria""; ""4.3 Engine-Out Maneuver Requirements FAR 25 Criteria""; ""4.4 Equations of Motion for Yawing Maneuvers""; ""Chapter 5. Flight in Turbulence""; ""5.1 Sharp-Edge Gust Criteria Based on Wing Loading""; ""5.2 Revised Gust Criteria Using Airplane Mass Ratio""; ""5.3 FAR/JAR Discrete Gust Design Criteria""; ""5.4 Continuous Turbulence Gust Loads Criteria""; ""5.5 Vertical Discrete Gust Considerations""; ""5.6 Transient Lift Functions"" ""5.7 Vertical Gust Continuous Turbulence Considerations""""5.8 Multiple DOF Analyses""; ""5.9 Lateral Gust Considerations""; ""5.10 Oblique Gusts""; ""5.11 Head-On Gusts""; ""Chapter 6. Landing Loads""; ""6.1 Criteria per FAR/JAR 25.473""; ""6.2 Landing Speed Calculations""; ""6.3 Two-Point Landing Conditions""; ""6.4 Three-Point Landing Conditions""; ""6.5 One-Gear Landing Conditions""; ""6.6 Side Load Conditions""; ""6.7 Rebound Landing Conditions""; ""6.8 Landing Gear Shock Absorption and Drop Tests""; ""6.9 Elastic Airplane Analysis""; ""6.10 Automatic Ground Spoilers"" ""Chapter 7. Ground-Handling Loads""""7.1 Ground-Handling Conditions""; ""7.2 Static Load Conditions""; ""7.3 Taxi, Takeoff, and Landing Roll Conditions""; ""7.4 Braked-Roll Conditions""; ""7.5 Refused Takeoff Considerations""; ""7.6 Turning Conditions""; ""7.7 Towing Conditions""; ""7.8 Jacking Loads per FAR/JAR 25.519""; ""7.9 Tethering Problem""; ""Chapter 8. Horizontal Tail Loads""; ""8.1 Horizontal Tail Design Load Envelopes""; ""8.2 Balanced Maneuver Analysis""; ""8.3 Abrupt Unchecked Elevator Conditions""; ""8.4 Checked Maneuver Conditions""; ""8.5 Vertical Gust Conditions"" ""8.6 Unsymmetrical Load Conditions"" |
| Record Nr. | UNINA-9910457218703321 |
|
Lomax Ted L
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax
| Structural loads analysis for commercial transport aircraft [[electronic resource] ] : theory and practice / / Ted L. Lomax |
| Autore | Lomax Ted L |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 |
| Descrizione fisica | 1 online resource (297 p.) |
| Disciplina | 629.134/31 |
| Collana | AIAA education series |
| Soggetto topico |
Airframes - Design and construction
Structural dynamics Transport planes - Design and construction |
| ISBN |
1-60086-246-2
1-60086-118-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Nomenclature""; ""Chapter 1. Introduction""; ""1.1 Applicability of the Analysis""; ""1.2 Criteria""; ""1.3 Methodogy""; ""1.4 Static Aeroelastic Phenomena""; ""1.5 Sign Convention""; ""Chapter 2. Symmetrical Maneuvering Flight""; ""2.1 Symmetrical Maneuvering Flight Definition""; ""2.2 Symmetrical Maneuver Load Factors""; ""2.3 Steady-State Symmetrical Maneuvers""; ""2.4 Abrupt Pitching Maneuvers""; ""2.5 Abrupt Unchecked Pitch Maneuvers""; ""2.6 Abrupt Checked Maneuvers (Commercial Requirements)""
""2.7 Abrupt Checked Maneuvers (Military Requirements)""""2.8 Minimum Pitch Acceleration Requirements""; ""Chapter 3. Rolling Maneuvers""; ""3.1 Parameters Required for Structural Load Analyses""; ""3.2 Symmetrical Load Factors for Rolling Maneuvers""; ""3.3 Control Surface Deflections for Rolling Maneuvers""; ""3.4 Equations of Motion for Rolling Maneuvers""; ""3.5 Maximum Rolling Acceleration and Velocity Criteria""; ""3.6 Roll Termination Condition""; ""3.7 Nonlinear Lateral Control Inputs""; ""3.8 Aeroelastic Effects""; ""Chapter 4. Yawing Maneuvers"" ""4.1 Parameters Required for Structural Load Analyses""""4.2 Rudder Maneuver Requirements FAR 25 Criteria""; ""4.3 Engine-Out Maneuver Requirements FAR 25 Criteria""; ""4.4 Equations of Motion for Yawing Maneuvers""; ""Chapter 5. Flight in Turbulence""; ""5.1 Sharp-Edge Gust Criteria Based on Wing Loading""; ""5.2 Revised Gust Criteria Using Airplane Mass Ratio""; ""5.3 FAR/JAR Discrete Gust Design Criteria""; ""5.4 Continuous Turbulence Gust Loads Criteria""; ""5.5 Vertical Discrete Gust Considerations""; ""5.6 Transient Lift Functions"" ""5.7 Vertical Gust Continuous Turbulence Considerations""""5.8 Multiple DOF Analyses""; ""5.9 Lateral Gust Considerations""; ""5.10 Oblique Gusts""; ""5.11 Head-On Gusts""; ""Chapter 6. Landing Loads""; ""6.1 Criteria per FAR/JAR 25.473""; ""6.2 Landing Speed Calculations""; ""6.3 Two-Point Landing Conditions""; ""6.4 Three-Point Landing Conditions""; ""6.5 One-Gear Landing Conditions""; ""6.6 Side Load Conditions""; ""6.7 Rebound Landing Conditions""; ""6.8 Landing Gear Shock Absorption and Drop Tests""; ""6.9 Elastic Airplane Analysis""; ""6.10 Automatic Ground Spoilers"" ""Chapter 7. Ground-Handling Loads""""7.1 Ground-Handling Conditions""; ""7.2 Static Load Conditions""; ""7.3 Taxi, Takeoff, and Landing Roll Conditions""; ""7.4 Braked-Roll Conditions""; ""7.5 Refused Takeoff Considerations""; ""7.6 Turning Conditions""; ""7.7 Towing Conditions""; ""7.8 Jacking Loads per FAR/JAR 25.519""; ""7.9 Tethering Problem""; ""Chapter 8. Horizontal Tail Loads""; ""8.1 Horizontal Tail Design Load Envelopes""; ""8.2 Balanced Maneuver Analysis""; ""8.3 Abrupt Unchecked Elevator Conditions""; ""8.4 Checked Maneuver Conditions""; ""8.5 Vertical Gust Conditions"" ""8.6 Unsymmetrical Load Conditions"" |
| Record Nr. | UNINA-9910781404203321 |
|
Lomax Ted L
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
