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 |
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 |
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 |
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 |
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 | ||
|