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Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester
| Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester |
| Autore | Sóbester András |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2015 |
| Descrizione fisica | 1 online resource (246 p.) |
| Disciplina | 629.134/1 |
| Collana |
Aerospace Series
THEi Wiley ebooks |
| Soggetto topico |
Airframes
Aerodynamics |
| ISBN |
1-5231-2340-0
1-118-53473-5 1-118-53474-3 1-118-53471-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910132162503321 |
Sóbester András
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| Chichester, England : , : Wiley, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester
| Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester |
| Autore | Sóbester András |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2015 |
| Descrizione fisica | 1 online resource (246 p.) |
| Disciplina | 629.134/1 |
| Collana |
Aerospace Series
THEi Wiley ebooks |
| Soggetto topico |
Airframes
Aerodynamics |
| ISBN |
1-5231-2340-0
1-118-53473-5 1-118-53474-3 1-118-53471-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910820810803321 |
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Sóbester András
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| Chichester, England : , : Wiley, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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CleanEra : a collection of research projects for sustainable aviation / / by The CleanEra Team
| CleanEra : a collection of research projects for sustainable aviation / / by The CleanEra Team |
| Pubbl/distr/stampa | Amsterdam, [The Netherlands] : , : IOS Press, , 2015 |
| Descrizione fisica | 1 online resource (192 pages) : illustrations |
| Disciplina | 629.134/1 |
| Soggetto topico |
Airplanes - Design and construction - Environmental aspects
Aircraft exhaust emissions |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-61499-591-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910163538503321 |
| Amsterdam, [The Netherlands] : , : IOS Press, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Design and development of aircraft systems [[electronic resource] /] / Ian Moir, Allan Seabridge
| Design and development of aircraft systems [[electronic resource] /] / Ian Moir, Allan Seabridge |
| Autore | Moir I (Ian) |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Chichester, West Sussex : , : Wiley, , c2013 |
| Descrizione fisica | 1 online resource (596 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) | SeabridgeA. G (Allan G.) |
| Collana |
Aerospace series
THEi Wiley ebooks |
| Soggetto topico |
Aeronautics - Systems engineering
Airplanes - Design and construction |
| ISBN |
1-5231-1060-0
1-118-46915-1 1-118-46913-5 1-118-46914-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- The aircraft systems -- The design and development process -- Design drivers -- Systems architectures -- Systems integration -- Verification of system requirements -- Practical considerations -- Configuration control -- Aircraft system examples -- Power system issues -- Key characteristics of aircraft systems -- Conclusions. |
| Record Nr. | UNINA-9910141603103321 |
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Moir I (Ian)
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| Chichester, West Sussex : , : Wiley, , c2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Design and development of aircraft systems / / Ian Moir, Allan Seabridge
| Design and development of aircraft systems / / Ian Moir, Allan Seabridge |
| Autore | Moir I (Ian) |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Chichester, West Sussex : , : Wiley, , c2013 |
| Descrizione fisica | 1 online resource (596 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) | SeabridgeA. G (Allan G.) |
| Collana |
Aerospace series
THEi Wiley ebooks |
| Soggetto topico |
Aeronautics - Systems engineering
Airplanes - Design and construction |
| ISBN |
1-5231-1060-0
1-118-46915-1 1-118-46913-5 1-118-46914-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- The aircraft systems -- The design and development process -- Design drivers -- Systems architectures -- Systems integration -- Verification of system requirements -- Practical considerations -- Configuration control -- Aircraft system examples -- Power system issues -- Key characteristics of aircraft systems -- Conclusions. |
| Record Nr. | UNINA-9910819826603321 |
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Moir I (Ian)
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| Chichester, West Sussex : , : Wiley, , c2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner
| Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner |
| Autore | Nicolai Leland M (Leland Malcolm) |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 |
| Descrizione fisica | 1 online resource (931 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) |
CarichnerGrant
NicolaiLeland M (Leland Malcolm) |
| Collana | AIAA educational series |
| Soggetto topico |
Airplanes - Design and construction - History
Airships - Design and construction - History Aeronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-752-9
1-61344-046-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
COVER; TITLE; COPYRIGHT; FOREWORD; CONTENTS; LIST OF COLOR PLATES; PREFACE; Chapter 1: Introduction; Chapter 2: Review of Practical Aerodynamics; Chapter 3: Aircraft Performance Methods; Chapter 4: Aircraft Operating Envelope; Chapter 5: Preliminary Estimate of Takeoff Weight; Chapter 6: Estimating theTakeoff Wing Loading; Chapter 7: Selecting the Planform and Airfoil Section; Chapter 8: Preliminary Fuselage Sizing and Design; Chapter 9: High-Lift Devices; Chapter 10: Takeoff and Landing Analysis; Chapter 11: Preliminary Sizing of the Vertical and Horizontal Tails
Chapter 12: Designing for Survivability (Stealth)Chapter 13: Estimating Wing-Body Aerodynamics; Chapter 14: Propulsion System Fundamentals; Chapter 15: Turbine Engine Inlet Design; Chapter 16: Corrections forTurbine Engine Installation; Chapter 17: Propeller Propulsion Systems; Chapter 18: Propulsion System Thrust Sizing; Chapter 19: Structures and Materials; Chapter 20: Refined Weight Estimate; Chapter 21 Static Stability and Control; Chapter 22: Trim Drag and Maneuvering Flight; Chapter 23: Control Surface Sizing Criteria; Chapter 24: Life Cycle Cost; Chapter 25: Trade Studies and Sizing Appendix A: ConversionsAppendix B: Atmospheric Data; Appendix C: Isentropic Compressible Flow Functions; Appendix D: Normal Shock Functions for a Perfect Gas; Appendix E: Plane Oblique and Conical Shocks; Appendix F: NACA Airfoil Nomenclature and Data; Appendix G: Aerodynamic Data of Real Aircraft; Appendix H: Aerodynamics of Wing-Body Combinations; Appendix I: Aircraft Weights Data; Appendix J: Propulsion Data; Appendix K: Miscellaneous Data; INDEX; SUPPORTING MATERIALS |
| Record Nr. | UNINA-9910465014803321 |
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Nicolai Leland M (Leland Malcolm)
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| Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner
| Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner |
| Autore | Nicolai Leland M (Leland Malcolm) |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 |
| Descrizione fisica | 1 online resource (931 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) |
CarichnerGrant
NicolaiLeland M (Leland Malcolm) |
| Collana | AIAA educational series |
| Soggetto topico |
Airplanes - Design and construction - History
Airships - Design and construction - History Aeronautics |
| ISBN |
1-60086-752-9
1-61344-046-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
COVER; TITLE; COPYRIGHT; FOREWORD; CONTENTS; LIST OF COLOR PLATES; PREFACE; Chapter 1: Introduction; Chapter 2: Review of Practical Aerodynamics; Chapter 3: Aircraft Performance Methods; Chapter 4: Aircraft Operating Envelope; Chapter 5: Preliminary Estimate of Takeoff Weight; Chapter 6: Estimating theTakeoff Wing Loading; Chapter 7: Selecting the Planform and Airfoil Section; Chapter 8: Preliminary Fuselage Sizing and Design; Chapter 9: High-Lift Devices; Chapter 10: Takeoff and Landing Analysis; Chapter 11: Preliminary Sizing of the Vertical and Horizontal Tails
Chapter 12: Designing for Survivability (Stealth)Chapter 13: Estimating Wing-Body Aerodynamics; Chapter 14: Propulsion System Fundamentals; Chapter 15: Turbine Engine Inlet Design; Chapter 16: Corrections forTurbine Engine Installation; Chapter 17: Propeller Propulsion Systems; Chapter 18: Propulsion System Thrust Sizing; Chapter 19: Structures and Materials; Chapter 20: Refined Weight Estimate; Chapter 21 Static Stability and Control; Chapter 22: Trim Drag and Maneuvering Flight; Chapter 23: Control Surface Sizing Criteria; Chapter 24: Life Cycle Cost; Chapter 25: Trade Studies and Sizing Appendix A: ConversionsAppendix B: Atmospheric Data; Appendix C: Isentropic Compressible Flow Functions; Appendix D: Normal Shock Functions for a Perfect Gas; Appendix E: Plane Oblique and Conical Shocks; Appendix F: NACA Airfoil Nomenclature and Data; Appendix G: Aerodynamic Data of Real Aircraft; Appendix H: Aerodynamics of Wing-Body Combinations; Appendix I: Aircraft Weights Data; Appendix J: Propulsion Data; Appendix K: Miscellaneous Data; INDEX; SUPPORTING MATERIALS |
| Record Nr. | UNINA-9910789084903321 |
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Nicolai Leland M (Leland Malcolm)
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner
| Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner |
| Autore | Nicolai Leland M (Leland Malcolm) |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 |
| Descrizione fisica | 1 online resource (931 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) |
CarichnerGrant
NicolaiLeland M (Leland Malcolm) |
| Collana | AIAA educational series |
| Soggetto topico |
Airplanes - Design and construction - History
Airships - Design and construction - History Aeronautics |
| ISBN |
1-60086-752-9
1-61344-046-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
COVER; TITLE; COPYRIGHT; FOREWORD; CONTENTS; LIST OF COLOR PLATES; PREFACE; Chapter 1: Introduction; Chapter 2: Review of Practical Aerodynamics; Chapter 3: Aircraft Performance Methods; Chapter 4: Aircraft Operating Envelope; Chapter 5: Preliminary Estimate of Takeoff Weight; Chapter 6: Estimating theTakeoff Wing Loading; Chapter 7: Selecting the Planform and Airfoil Section; Chapter 8: Preliminary Fuselage Sizing and Design; Chapter 9: High-Lift Devices; Chapter 10: Takeoff and Landing Analysis; Chapter 11: Preliminary Sizing of the Vertical and Horizontal Tails
Chapter 12: Designing for Survivability (Stealth)Chapter 13: Estimating Wing-Body Aerodynamics; Chapter 14: Propulsion System Fundamentals; Chapter 15: Turbine Engine Inlet Design; Chapter 16: Corrections forTurbine Engine Installation; Chapter 17: Propeller Propulsion Systems; Chapter 18: Propulsion System Thrust Sizing; Chapter 19: Structures and Materials; Chapter 20: Refined Weight Estimate; Chapter 21 Static Stability and Control; Chapter 22: Trim Drag and Maneuvering Flight; Chapter 23: Control Surface Sizing Criteria; Chapter 24: Life Cycle Cost; Chapter 25: Trade Studies and Sizing Appendix A: ConversionsAppendix B: Atmospheric Data; Appendix C: Isentropic Compressible Flow Functions; Appendix D: Normal Shock Functions for a Perfect Gas; Appendix E: Plane Oblique and Conical Shocks; Appendix F: NACA Airfoil Nomenclature and Data; Appendix G: Aerodynamic Data of Real Aircraft; Appendix H: Aerodynamics of Wing-Body Combinations; Appendix I: Aircraft Weights Data; Appendix J: Propulsion Data; Appendix K: Miscellaneous Data; INDEX; SUPPORTING MATERIALS |
| Record Nr. | UNINA-9910824305403321 |
|
Nicolai Leland M (Leland Malcolm)
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Introduction to aeronautics [[electronic resource] ] : a design perspective / / Steven A. Brandt ... [et al.]
| Introduction to aeronautics [[electronic resource] ] : a design perspective / / Steven A. Brandt ... [et al.] |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2004 |
| Descrizione fisica | 1 online resource (530 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) | BrandtSteven A. <1953-> |
| Collana | AIAA education series |
| Soggetto topico |
Airplanes - Design and construction
Aeronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60086-072-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword to the Second Edition""; ""Foreword to the First Edition""; ""Table of Contents""; ""Preface""; ""Acknowledgments""; ""Nomenclature""; ""Chapter 1. Design Thinking""; ""1.1 Introduction""; ""1.2 Design Method""; ""1.3 Design Example""; ""1.4 Design and Aeronautics""; ""1.5 Brief History of Aircraft Design""; ""1.6 Conclusion""; ""1.7 Chapter Summary""; ""1.8 More Details""; ""References""; ""Problems""; ""Chapter 2. Operating Environment""; ""2.1 Design Motivation""; ""2.2 Characteristics of the Atmosphere""; ""2.3 Pressure Measurement""
""2.4 Standard Atmosphere""""2.5 Common Uses of the Standard Atmosphere""; ""2.6 Chapter Summary""; ""2.7 More Details�Molecular Collisions and Aerodynamics""; ""Reference""; ""Problems""; ""Chapter 3. Aerodynamics and Airfoils""; ""3.1 Design Motivation""; ""3.2 Basic Aerodynamics""; ""3.3 Basic Aerodynamics Applications""; ""3.4 Viscous Flow""; ""3.5 Airfoil Characteristics""; ""3.6 Chapter Summary""; ""3.7 More Details""; ""References""; ""Problems""; ""Chapter 4. Wings and Airplanes""; ""4.1 Design Motivation""; ""4.2 Wings""; ""4.3 High-Lift Devices""; ""4.4 Whole Aircraft Lift"" ""4.5 Whole Aircraft Drag and Drag Polar""""4.6 Mach-Number Effects""; ""4.7 Chapter Summary""; ""4.8 More Details""; ""4.9 Whole Aircraft Analysis Example""; ""References""; ""Problems""; ""Chapter 5. Performance""; ""5.1 Design Motivation""; ""5.2 Equations of Motion""; ""5.3 Propulsion""; ""5.4 Drag Curves""; ""5.5 Lift-to-Drag Ratio""; ""5.6 Power Curves""; ""5.7 Curve Shifts""; ""5.8 Glides""; ""5.9 Climbs""; ""5.10 Range and Endurance""; ""5.11 Takeoff and Landing""; ""5.12 Turns""; ""5.13 V�n Diagrams""; ""5.14 Energy Height and Specific Excess Power""; ""5.15 Chapter Summary"" ""5.16 More Details�Maneuverability Diagrams and Constraint Analysis""""5.17 Performance Analysis Example""; ""References""; ""Problems""; ""Chapter 6. Stability and Control""; ""6.1 Design Motivation""; ""6.2 Language""; ""6.3 Longitudinal Control Analysis""; ""6.4 Longitudinal Stability""; ""6.5 Dynamic Longitudinal Stability""; ""6.6 Lateral-Directional Stability""; ""6.7 Dynamic Lateral-Directional Stability""; ""6.8 Chapter Summary""; ""6.9 More Details�Calculating Stability Parameters""; ""6.10 Stability and Control Analysis Example: F-16A and F-16C""; ""Reference""; ""Problems"" ""Chapter 7. Structures""""7.1 Design Motivation""; ""7.2 Solid Mechanics""; ""7.3 Types of Stress""; ""7.4 Loads""; ""7.5 Structural Layout""; ""7.6 Materials""; ""7.7 Component Sizing""; ""7.8 Structural Sizing Example""; ""7.9 Weight Estimates""; ""7.10 Finite Element Analysis""; ""7.11 Chapter Summary""; ""References""; ""Problems""; ""Chapter 8. Sizing""; ""8.1 Design Motivation""; ""8.2 Internal Layout""; ""8.3 Structures and Weight""; ""8.4 Geometry Constraints""; ""8.5 Mission Analysis""; ""8.6 Sizing Equation""; ""8.7 Weight Fraction Method""; ""8.8 Weight and Balance"" ""8.9 Mission Analysis and Sizing Example"" |
| Record Nr. | UNINA-9910454417303321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2004 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Introduction to aeronautics [[electronic resource] ] : a design perspective / / Steven A. Brandt ... [et al.]
| Introduction to aeronautics [[electronic resource] ] : a design perspective / / Steven A. Brandt ... [et al.] |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2004 |
| Descrizione fisica | 1 online resource (530 p.) |
| Disciplina | 629.134/1 |
| Altri autori (Persone) | BrandtSteven A. <1953-> |
| Collana | AIAA education series |
| Soggetto topico |
Airplanes - Design and construction
Aeronautics |
| ISBN | 1-60086-072-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword to the Second Edition""; ""Foreword to the First Edition""; ""Table of Contents""; ""Preface""; ""Acknowledgments""; ""Nomenclature""; ""Chapter 1. Design Thinking""; ""1.1 Introduction""; ""1.2 Design Method""; ""1.3 Design Example""; ""1.4 Design and Aeronautics""; ""1.5 Brief History of Aircraft Design""; ""1.6 Conclusion""; ""1.7 Chapter Summary""; ""1.8 More Details""; ""References""; ""Problems""; ""Chapter 2. Operating Environment""; ""2.1 Design Motivation""; ""2.2 Characteristics of the Atmosphere""; ""2.3 Pressure Measurement""
""2.4 Standard Atmosphere""""2.5 Common Uses of the Standard Atmosphere""; ""2.6 Chapter Summary""; ""2.7 More Details�Molecular Collisions and Aerodynamics""; ""Reference""; ""Problems""; ""Chapter 3. Aerodynamics and Airfoils""; ""3.1 Design Motivation""; ""3.2 Basic Aerodynamics""; ""3.3 Basic Aerodynamics Applications""; ""3.4 Viscous Flow""; ""3.5 Airfoil Characteristics""; ""3.6 Chapter Summary""; ""3.7 More Details""; ""References""; ""Problems""; ""Chapter 4. Wings and Airplanes""; ""4.1 Design Motivation""; ""4.2 Wings""; ""4.3 High-Lift Devices""; ""4.4 Whole Aircraft Lift"" ""4.5 Whole Aircraft Drag and Drag Polar""""4.6 Mach-Number Effects""; ""4.7 Chapter Summary""; ""4.8 More Details""; ""4.9 Whole Aircraft Analysis Example""; ""References""; ""Problems""; ""Chapter 5. Performance""; ""5.1 Design Motivation""; ""5.2 Equations of Motion""; ""5.3 Propulsion""; ""5.4 Drag Curves""; ""5.5 Lift-to-Drag Ratio""; ""5.6 Power Curves""; ""5.7 Curve Shifts""; ""5.8 Glides""; ""5.9 Climbs""; ""5.10 Range and Endurance""; ""5.11 Takeoff and Landing""; ""5.12 Turns""; ""5.13 V�n Diagrams""; ""5.14 Energy Height and Specific Excess Power""; ""5.15 Chapter Summary"" ""5.16 More Details�Maneuverability Diagrams and Constraint Analysis""""5.17 Performance Analysis Example""; ""References""; ""Problems""; ""Chapter 6. Stability and Control""; ""6.1 Design Motivation""; ""6.2 Language""; ""6.3 Longitudinal Control Analysis""; ""6.4 Longitudinal Stability""; ""6.5 Dynamic Longitudinal Stability""; ""6.6 Lateral-Directional Stability""; ""6.7 Dynamic Lateral-Directional Stability""; ""6.8 Chapter Summary""; ""6.9 More Details�Calculating Stability Parameters""; ""6.10 Stability and Control Analysis Example: F-16A and F-16C""; ""Reference""; ""Problems"" ""Chapter 7. Structures""""7.1 Design Motivation""; ""7.2 Solid Mechanics""; ""7.3 Types of Stress""; ""7.4 Loads""; ""7.5 Structural Layout""; ""7.6 Materials""; ""7.7 Component Sizing""; ""7.8 Structural Sizing Example""; ""7.9 Weight Estimates""; ""7.10 Finite Element Analysis""; ""7.11 Chapter Summary""; ""References""; ""Problems""; ""Chapter 8. Sizing""; ""8.1 Design Motivation""; ""8.2 Internal Layout""; ""8.3 Structures and Weight""; ""8.4 Geometry Constraints""; ""8.5 Mission Analysis""; ""8.6 Sizing Equation""; ""8.7 Weight Fraction Method""; ""8.8 Weight and Balance"" ""8.9 Mission Analysis and Sizing Example"" |
| Record Nr. | UNINA-9910782755303321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2004 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
