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Aeronautical engineer's data book [[electronic resource] /] / Clifford Matthews
| Aeronautical engineer's data book [[electronic resource] /] / Clifford Matthews |
| Autore | Matthews Clifford |
| Pubbl/distr/stampa | Oxford ; ; Boston, : Butterworth-Heinemann, 2002 |
| Descrizione fisica | 1 online resource (282 p.) |
| Disciplina | 629.13/002/12 |
| Soggetto topico | Aeronautics |
| ISBN |
1-281-04944-1
9786611049447 0-08-048828-5 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | ger |
| Nota di contenuto |
Front Cover; Aeronautical Engineer's Data Book; Copyright Page; Contents; Preface; Acknowledgements; Disclaimer; Chapter 1. Important regulations and directives; Chapter 2. Fundamental dimensions and units; 2.1 The Greek alphabet; 2.2 Units systems; 2.3 Conversions; 2.4 Consistency of units; 2.5 Foolproof conversions: using unity brackets; 2.6 Imperial-metric conversions; 2.7 Dimensional analysis; 2.8 Essential mathematics; 2.9 Useful references and standards; Chapter 3. Symbols and notations; 3.1 Parameters and constants; 3.2 Weights of gases; 3.3 Densities of liquids at 0°C
3.4 Notation: aerodynamics and fluid mechanics3.5 The International Standard Atmosphere (ISA); Chapter 4. Aeronautical definitions; 4.1 Forces and moments; 4.2 Basic aircraft terminology; 4.3 Helicopter terminology; 4.4 Common aviation terms; 4.5 Airspace terms; Chapter 5. Basic fluid mechanics; 5.1 Basic properties; 5.2 Flow equations; 5.3 Flow regimes; 5.4 Boundary layers; 5.5 Isentropic flow; 5.6 Compressible 1D flow; 5.7 Normal shock waves; 5.8 Axisymmetric flows; 5.9 Drag coefficients; Chapter 6. Basic aerodynamics; 6.1 General airfoil theory; 6.2 Airfoil coefficients 6.3 Pressure distributions6.4 Aerodynamic centre; 6.5 Centre of pressure; 6.6 Supersonic conditions; 6.7 Wing loading: semi-ellipse assumption; Chapter 7. Principles of flight dynamics; 7.1 Flight dynamics-conceptual breakdown; 7.2 Axes notation; 7.3 The generalized force equations; 7.4 The generalized moment equations; 7.5 Non-linear equations of motion; 7.6 The linearized equations of motion; 7.7 Stability; Chapter 8. Principles of propulsion; 8.1 Propellers; 8.2 The gas turbine engine: general principles; 8.3 Engine data lists; 8.4 Aero engine terminology; 8.5 Power ratings Chapter 9. Aircraft performance9.1 Aircraft roles and operational profile; 9.2 Aircraft range and endurance; 9.3 Aircraft design studies; 9.4 Aircraft noise; 9.5 Aircraft emissions; Chapter 10. Aircraft design and construction; 10.1 Basic design configuration; 10.2 Materials of construction; 10.3 Helicopter design; 10.4 Helicopter design studies; Chapter 11. Airport design and compatibility; 11.1 Basics of airport design; 11.2 Runway pavements; 11.3 Airport traffic data; 11.4 FAA-AAS Airport documents; 11.5 Worldwide airport geographical data; 11.6 Airport reference sources and bibliography Chapter 12. Basic mechanical design12.1 Engineering abbreviations; 12.2 Preferred numbers and preferred sizes; 12.3 Datums and tolerances-principles; 12.4 Toleranced dimensions; 12.5 Limits and fits; 12.6 Surface finish; 12.7 Computer aided engineering; Chapter 13. Reference sources; 13.1 Websites; 13.2 Fluid mechanics and aerodynamics; 13.3 Manufacturing/materials/structures; 13.4 Aircraft sizing/multidisciplinary design; 13.5 Helicopter technology; 13.6 Flying wings; 13.7 Noise; 13.8 Landing gear; 13.9 Aircraft operations; 13.10 Propulsion Appendix 1. Aerodynamic stability and control derivatives |
| Record Nr. | UNINA-9910783930603321 |
Matthews Clifford
|
||
| Oxford ; ; Boston, : Butterworth-Heinemann, 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aeronautical engineers' data book [[electronic resource] /] / Clifford Matthews
| Aeronautical engineers' data book [[electronic resource] /] / Clifford Matthews |
| Autore | Matthews Clifford |
| Pubbl/distr/stampa | Oxford ; ; Boston, : Butterworth-Heinemann, 2002 |
| Descrizione fisica | 1 online resource (282 p.) |
| Disciplina | 629.13/002/12 |
| Soggetto topico | Aeronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-281-04944-1
9786611049447 0-08-048828-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | ger |
| Nota di contenuto |
Front Cover; Aeronautical Engineer's Data Book; Copyright Page; Contents; Preface; Acknowledgements; Disclaimer; Chapter 1. Important regulations and directives; Chapter 2. Fundamental dimensions and units; 2.1 The Greek alphabet; 2.2 Units systems; 2.3 Conversions; 2.4 Consistency of units; 2.5 Foolproof conversions: using unity brackets; 2.6 Imperial-metric conversions; 2.7 Dimensional analysis; 2.8 Essential mathematics; 2.9 Useful references and standards; Chapter 3. Symbols and notations; 3.1 Parameters and constants; 3.2 Weights of gases; 3.3 Densities of liquids at 0°C
3.4 Notation: aerodynamics and fluid mechanics3.5 The International Standard Atmosphere (ISA); Chapter 4. Aeronautical definitions; 4.1 Forces and moments; 4.2 Basic aircraft terminology; 4.3 Helicopter terminology; 4.4 Common aviation terms; 4.5 Airspace terms; Chapter 5. Basic fluid mechanics; 5.1 Basic properties; 5.2 Flow equations; 5.3 Flow regimes; 5.4 Boundary layers; 5.5 Isentropic flow; 5.6 Compressible 1D flow; 5.7 Normal shock waves; 5.8 Axisymmetric flows; 5.9 Drag coefficients; Chapter 6. Basic aerodynamics; 6.1 General airfoil theory; 6.2 Airfoil coefficients 6.3 Pressure distributions6.4 Aerodynamic centre; 6.5 Centre of pressure; 6.6 Supersonic conditions; 6.7 Wing loading: semi-ellipse assumption; Chapter 7. Principles of flight dynamics; 7.1 Flight dynamics-conceptual breakdown; 7.2 Axes notation; 7.3 The generalized force equations; 7.4 The generalized moment equations; 7.5 Non-linear equations of motion; 7.6 The linearized equations of motion; 7.7 Stability; Chapter 8. Principles of propulsion; 8.1 Propellers; 8.2 The gas turbine engine: general principles; 8.3 Engine data lists; 8.4 Aero engine terminology; 8.5 Power ratings Chapter 9. Aircraft performance9.1 Aircraft roles and operational profile; 9.2 Aircraft range and endurance; 9.3 Aircraft design studies; 9.4 Aircraft noise; 9.5 Aircraft emissions; Chapter 10. Aircraft design and construction; 10.1 Basic design configuration; 10.2 Materials of construction; 10.3 Helicopter design; 10.4 Helicopter design studies; Chapter 11. Airport design and compatibility; 11.1 Basics of airport design; 11.2 Runway pavements; 11.3 Airport traffic data; 11.4 FAA-AAS Airport documents; 11.5 Worldwide airport geographical data; 11.6 Airport reference sources and bibliography Chapter 12. Basic mechanical design12.1 Engineering abbreviations; 12.2 Preferred numbers and preferred sizes; 12.3 Datums and tolerances-principles; 12.4 Toleranced dimensions; 12.5 Limits and fits; 12.6 Surface finish; 12.7 Computer aided engineering; Chapter 13. Reference sources; 13.1 Websites; 13.2 Fluid mechanics and aerodynamics; 13.3 Manufacturing/materials/structures; 13.4 Aircraft sizing/multidisciplinary design; 13.5 Helicopter technology; 13.6 Flying wings; 13.7 Noise; 13.8 Landing gear; 13.9 Aircraft operations; 13.10 Propulsion Appendix 1. Aerodynamic stability and control derivatives |
| Record Nr. | UNINA-9910451109303321 |
|
Matthews Clifford
|
||
| Oxford ; ; Boston, : Butterworth-Heinemann, 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aeronautical engineers' data book / / Clifford Matthews
| Aeronautical engineers' data book / / Clifford Matthews |
| Autore | Matthews Clifford |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Oxford ; ; Boston, : Butterworth-Heinemann, 2002 |
| Descrizione fisica | 1 online resource (282 p.) |
| Disciplina | 629.13/002/12 |
| Soggetto topico | Aeronautics |
| ISBN |
9786611049447
9781281049445 1281049441 9780080488288 0080488285 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | ger |
| Nota di contenuto |
Front Cover; Aeronautical Engineer's Data Book; Copyright Page; Contents; Preface; Acknowledgements; Disclaimer; Chapter 1. Important regulations and directives; Chapter 2. Fundamental dimensions and units; 2.1 The Greek alphabet; 2.2 Units systems; 2.3 Conversions; 2.4 Consistency of units; 2.5 Foolproof conversions: using unity brackets; 2.6 Imperial-metric conversions; 2.7 Dimensional analysis; 2.8 Essential mathematics; 2.9 Useful references and standards; Chapter 3. Symbols and notations; 3.1 Parameters and constants; 3.2 Weights of gases; 3.3 Densities of liquids at 0°C
3.4 Notation: aerodynamics and fluid mechanics3.5 The International Standard Atmosphere (ISA); Chapter 4. Aeronautical definitions; 4.1 Forces and moments; 4.2 Basic aircraft terminology; 4.3 Helicopter terminology; 4.4 Common aviation terms; 4.5 Airspace terms; Chapter 5. Basic fluid mechanics; 5.1 Basic properties; 5.2 Flow equations; 5.3 Flow regimes; 5.4 Boundary layers; 5.5 Isentropic flow; 5.6 Compressible 1D flow; 5.7 Normal shock waves; 5.8 Axisymmetric flows; 5.9 Drag coefficients; Chapter 6. Basic aerodynamics; 6.1 General airfoil theory; 6.2 Airfoil coefficients 6.3 Pressure distributions6.4 Aerodynamic centre; 6.5 Centre of pressure; 6.6 Supersonic conditions; 6.7 Wing loading: semi-ellipse assumption; Chapter 7. Principles of flight dynamics; 7.1 Flight dynamics-conceptual breakdown; 7.2 Axes notation; 7.3 The generalized force equations; 7.4 The generalized moment equations; 7.5 Non-linear equations of motion; 7.6 The linearized equations of motion; 7.7 Stability; Chapter 8. Principles of propulsion; 8.1 Propellers; 8.2 The gas turbine engine: general principles; 8.3 Engine data lists; 8.4 Aero engine terminology; 8.5 Power ratings Chapter 9. Aircraft performance9.1 Aircraft roles and operational profile; 9.2 Aircraft range and endurance; 9.3 Aircraft design studies; 9.4 Aircraft noise; 9.5 Aircraft emissions; Chapter 10. Aircraft design and construction; 10.1 Basic design configuration; 10.2 Materials of construction; 10.3 Helicopter design; 10.4 Helicopter design studies; Chapter 11. Airport design and compatibility; 11.1 Basics of airport design; 11.2 Runway pavements; 11.3 Airport traffic data; 11.4 FAA-AAS Airport documents; 11.5 Worldwide airport geographical data; 11.6 Airport reference sources and bibliography Chapter 12. Basic mechanical design12.1 Engineering abbreviations; 12.2 Preferred numbers and preferred sizes; 12.3 Datums and tolerances-principles; 12.4 Toleranced dimensions; 12.5 Limits and fits; 12.6 Surface finish; 12.7 Computer aided engineering; Chapter 13. Reference sources; 13.1 Websites; 13.2 Fluid mechanics and aerodynamics; 13.3 Manufacturing/materials/structures; 13.4 Aircraft sizing/multidisciplinary design; 13.5 Helicopter technology; 13.6 Flying wings; 13.7 Noise; 13.8 Landing gear; 13.9 Aircraft operations; 13.10 Propulsion Appendix 1. Aerodynamic stability and control derivatives |
| Record Nr. | UNINA-9910958777303321 |
|
Matthews Clifford
|
||
| Oxford ; ; Boston, : Butterworth-Heinemann, 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||