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Theory and practice of aircraft performance / / Ajoy Kumar Kundu, Queens University Belfast, Belfast, UK, Mark Price, Queens University Belfast, Belfast, UK, David Riordan, Bombardier Aerospace, Montreal, Canada
| Theory and practice of aircraft performance / / Ajoy Kumar Kundu, Queens University Belfast, Belfast, UK, Mark Price, Queens University Belfast, Belfast, UK, David Riordan, Bombardier Aerospace, Montreal, Canada |
| Autore | Kundu Ajoy Kumar <1932-> |
| Edizione | [Second edition.] |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (991 p.) |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico | Airplanes - Performance |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-119-07419-3
1-119-07418-5 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page; Table of Contents; Preface; Series Preface; Road Map of the Book; Organization; Suggested Structure for the Coursework; Acknowledgements; By A.K. Kundu; By Mark Price; By David Riordan; Nomenclature; CHAPTER 1: Introduction; 1.1 Overview; 1.2 Brief Historical Background; 1.3 Current Aircraft Design Status; 1.4 Future Trends; 1.5 Airworthiness Requirements; 1.6 Current Aircraft Performance Analyses Levels; 1.7 Market Survey; 1.8 Typical Design Process; 1.9 Classroom Learning Process; 1.10 Cost Implications; 1.11 Units and Dimensions; 1.12 Use of Semi-empirical Relations and Graphs
1.13 How Do Aircraft Fly?1.14 Anatomy of Aircraft; 1.15 Aircraft Motion and Forces; References; CHAPTER 2: Aerodynamic and Aircraft Design Considerations; 2.1 Overview; 2.2 Introduction; 2.3 Atmosphere; 2.4 Airflow Behaviour: Laminar and Turbulent; 2.5 Aerofoil; 2.6 Generation of Lift; 2.7 Types of Stall; 2.8 Comparison of Three NACA Aerofoils; 2.9 High-Lift Devices; 2.10 Transonic Effects - Area Rule; 2.11 Wing Aerodynamics; 2.12 Aspect Ratio Correction of 2D-Aerofoil Characteristics for 3D-Finite Wing; 2.13 Wing Definitions; 2.14 Mean Aerodynamic Chord 2.15 Compressibility Effect: Wing Sweep2.16 Wing-Stall Pattern and Wing Twist; 2.17 Influence of Wing Area and Span on Aerodynamics; 2.18 Empennage; 2.19 Fuselage; 2.20 Nacelle and Intake; 2.21 Speed Brakes and Dive Brakes; References; CHAPTER 3: Air Data Measuring Instruments, Systems and Parameters; 3.1 Overview; 3.2 Introduction; 3.3 Aircraft Speed; 3.4 Air Data Instruments; 3.5 Aircraft Flight-Deck (Cockpit) Layout; 3.6 Aircraft Mass (Weights) and Centre of Gravity; 3.7 Noise Emissions; 3.8 Engine-Exhaust Emissions; 3.9 Aircraft Systems; 3.10 Low Observable (LO) Aircraft Configuration ReferencesCHAPTER 4: Equations of Motion for a Flat Stationary Earth; 4.1 Overview; 4.2 Introduction; 4.3 Definitions of Frames of Reference (Flat Stationary E arth) and Nomenclature Used; 4.4 Eulerian Angles; 4.5 Simplified Equations of Motion for a Flat Stationary Earth; Reference; CHAPTER 5: Aircraft Load; 5.1 Overview; 5.2 Introduction; 5.3 Flight Manoeuvres; 5.4 Aircraft Loads; 5.5 Theory and Definitions; 5.6 Limits - Loads and Speeds; 5.7 V-nDiagram; 5.8 Gust Envelope; Reference; CHAPTER 6: Stability Considerations Affecting Aircraft Performance; 6.1 Overview; 6.2 Introduction 6.3 Static and Dynamic Stability6.4 Theory; 6.5 Current Statistical Trends for Horizontal and Vertical Tail Coefficients; 6.6 Inherent Aircraft Motions as Characteristics of Design; 6.7 Spinning; 6.8 Summary of Design Considerations for Stability; References; CHAPTER 7: Aircraft Power Plant and Integration; 7.1 Overview; 7.2 Background; 7.3 Definitions; 7.4 Air-Breathing Aircraft Engine Types; 7.5 Simplified Representation of Gas Turbine (Brayton/Joule) Cycle; 7.6 Formulation/Theory - Isentropic Case; 7.7 Engine Integration to Aircraft - Installation Effects; 7.8 Intake/Nozzle Design 7.9 Exhaust Nozzle and Thrust Reverser |
| Record Nr. | UNINA-9910465790303321 |
Kundu Ajoy Kumar <1932->
|
||
| Chichester, England : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Theory and practice of aircraft performance / / Ajoy Kumar Kundu, Queens University Belfast, Belfast, UK, Mark Price, Queens University Belfast, Belfast, UK, David Riordan, Bombardier Aerospace, Montreal, Canada
| Theory and practice of aircraft performance / / Ajoy Kumar Kundu, Queens University Belfast, Belfast, UK, Mark Price, Queens University Belfast, Belfast, UK, David Riordan, Bombardier Aerospace, Montreal, Canada |
| Autore | Kundu Ajoy Kumar <1934-> |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (991 pages) : illustrations |
| Disciplina | 629.132/3 |
| Collana | Aerospace Series. |
| Soggetto topico | Airplanes - Performance |
| ISBN |
1-119-07418-5
1-119-07419-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910795948103321 |
|
Kundu Ajoy Kumar <1934->
|
||
| Chichester, England : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Theory and practice of aircraft performance / / Ajoy Kumar Kundu, Queens University Belfast, Belfast, UK, Mark Price, Queens University Belfast, Belfast, UK, David Riordan, Bombardier Aerospace, Montreal, Canada
| Theory and practice of aircraft performance / / Ajoy Kumar Kundu, Queens University Belfast, Belfast, UK, Mark Price, Queens University Belfast, Belfast, UK, David Riordan, Bombardier Aerospace, Montreal, Canada |
| Autore | Kundu Ajoy Kumar <1934-> |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (991 pages) : illustrations |
| Disciplina | 629.132/3 |
| Collana | Aerospace Series. |
| Soggetto topico | Airplanes - Performance |
| ISBN |
1-119-07418-5
1-119-07419-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910807990803321 |
|
Kundu Ajoy Kumar <1934->
|
||
| Chichester, England : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||