Commercial airplane design principles
Commercial Airplane Design Principles is a succinct, focused text covering all the information required at the preliminary stage of aircraft design: initial sizing and weight estimation, fuselage design, engine selection, aerodynamic analysis, stability and control, drag estimation, performance an...
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| Formato: | Libro electrónico |
| Idioma: | Inglés |
| Publicado: |
Oxford, [England] ; Waltham, [Massachusetts] :
Butterworth-Heinemann
2014.
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| Edición: | 1st edition |
| Colección: | Elsevier aerospace engineering series Commercial airplane design principles
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| Materias: | |
| Ver en Biblioteca Universitat Ramon Llull: | https://discovery.url.edu/permalink/34CSUC_URL/1im36ta/alma991009629744606719 |
Tabla de Contenidos:
- Half Title; Title Page; Copyright; Contents; Preface; Introduction and Outline of an Airplane Design Report; 1 Market Survey and Mission Specification; 1.1 A growing market for commercial aircraft; 1.2 Technology drivers; 1.2.1 Fuel efficiency; 1.2.2 Weight reduction; 1.2.3 Drag reduction; 1.2.4 Engine design; 1.2.5 Carbon footprint; 1.2.6 Biofuels; 1.2.7 Alternative fuels and power sources; 1.2.8 Noise and vibration; 1.3 Cargo aircraft; 1.4 Design summary; 1.4.1 Mission specification; 1.4.2 The market survey; References; 2 Preliminary Weight Estimation; 2.1 The mission specification
- 2.2 The mission profile2.3 Weight components; 2.3.1 Gross, takeoff, and operating empty weights; 2.3.2 Passenger and crew weights; 2.3.3 Cargo weight; 2.3.4 Fuel weight; 2.3.5 Fuel consumption by mission segment; 2.3.6 Fuel consumption in segments other than cruise; 2.3.7 Fuel consumption in cruise; 2.3.8 Selection of cruise performance characteristics; 2.4 Empty weight trends; 2.5 Fuel characteristics; 2.6 Estimation of the takeoff and empty weights; 2.6.1 New materials for weight reduction; 2.7 Weight estimation for turboprop-powered aircraft
- 2.7.1 Fuel weight estimation for turboprop airliners2.7.2 Empty weight estimation for turboprop airliners; 2.8 Design summary; 2.9 Nomenclature; 2.9.1 Subscript; References; 3 Fuselage Design; 3.1 Introduction; 3.2 Commercial aircraft cabin volume and pressure; 3.2.1 Cabin volume; 3.2.2 Cabin pressure; 3.3 General cabin layout; 3.4 Cabin cross-section; 3.5 Estimation of fuselage width; 3.6 Estimation of fuselage length; 3.7 Influence of fuselage fineness ratio; 3.7.1 Fuselage effects on drag; 3.7.2 Fuselage effect on lift; 3.8 Estimation of nose cone and tail cone length; 3.9 Cargo containers
- 3.10 Emergency exits3.11 Recent developments in fuselage design; 3.12 Design summary; References; 4 Engine Selection; 4.1 Introduction; 4.2 Landing requirements; 4.3 Wing loading in landing; 4.4 Landing field length; 4.5 Wing loading in takeoff; 4.6 Takeoff distance; 4.7 Cruise requirements; 4.8 Construction of the engine selection design chart; 4.9 Flight test data for landing and power approach; 4.10 Turbojet and turbofan engines; 4.10.1 Dual shaft turbojet; 4.10.2 Dual shaft high bypass turbofan; 4.10.3 Determination of net thrust; 4.10.4 Net thrust in takeoff; 4.10.5 Net thrust in cruise
- 4.10.6 Specific fuel consumption in cruise4.11 Turboprops; 4.11.1 Takeoff distance; 4.11.2 Turboprop cruise requirements; 4.11.3 Estimating takeoff thrust and specific fuel consumption; 4.12 Engine-out operation and balanced field length; 4.13 Design summary; 4.14 Nomenclature; References; 5 Wing Design; 5.1 General wing planform characteristics; 5.1.1 The straight-tapered wing planform; 5.1.2 Cranked wing planform; 5.1.3 Wing dihedral; 5.2 General airfoil characteristics; 5.2.1 Airfoil sections; 5.2.2 Airfoils at angle of attack; 5.2.3 Airfoil selection
- 5.2.4 Compressibility effects on airfoils
