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Commercial airplane design principles / / Pasquale M. Sforza
| Commercial airplane design principles / / Pasquale M. Sforza |
| Autore | Sforza P. M |
| Edizione | [1st edition] |
| Pubbl/distr/stampa | Oxford, [England] ; ; Waltham, [Massachusetts] : , : Butterworth-Heinemann, , 2014 |
| Descrizione fisica | 1 online resource (623 p.) |
| Disciplina | 629.1341 |
| Collana | Elsevier aerospace engineering series Commercial airplane design principles |
| Soggetto topico |
Airplanes - Design and construction
Aerospace engineering Aircraft industry |
| Soggetto genere / forma | Electronic books. |
| ISBN | 0-12-419977-1 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
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 |
| Record Nr. | UNINA-9910464871403321 |
Sforza P. M
|
||
| Oxford, [England] ; ; Waltham, [Massachusetts] : , : Butterworth-Heinemann, , 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Commercial airplane design principles / / Pasquale M. Sforza
| Commercial airplane design principles / / Pasquale M. Sforza |
| Autore | Sforza P. M |
| Edizione | [1st edition] |
| Pubbl/distr/stampa | Oxford, [England] ; ; Waltham, [Massachusetts] : , : Butterworth-Heinemann, , 2014 |
| Descrizione fisica | 1 online resource (623 p.) |
| Disciplina | 629.1341 |
| Collana | Elsevier aerospace engineering series Commercial airplane design principles |
| Soggetto topico |
Airplanes - Design and construction
Aerospace engineering Aircraft industry |
| ISBN | 0-12-419977-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
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 |
| Record Nr. | UNINA-9910789118803321 |
|
Sforza P. M
|
||
| Oxford, [England] ; ; Waltham, [Massachusetts] : , : Butterworth-Heinemann, , 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Commercial airplane design principles / / Pasquale M. Sforza
| Commercial airplane design principles / / Pasquale M. Sforza |
| Autore | Sforza P. M |
| Edizione | [1st edition] |
| Pubbl/distr/stampa | Oxford, [England] ; ; Waltham, [Massachusetts] : , : Butterworth-Heinemann, , 2014 |
| Descrizione fisica | 1 online resource (623 p.) |
| Disciplina | 629.1341 |
| Collana | Elsevier aerospace engineering series Commercial airplane design principles |
| Soggetto topico |
Airplanes - Design and construction
Aerospace engineering Aircraft industry |
| ISBN | 0-12-419977-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
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 |
| Record Nr. | UNINA-9910818892303321 |
|
Sforza P. M
|
||
| Oxford, [England] ; ; Waltham, [Massachusetts] : , : Butterworth-Heinemann, , 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Theory of aerospace propulsion [[electronic resource] /] / Pasquale M. Sforza
| Theory of aerospace propulsion [[electronic resource] /] / Pasquale M. Sforza |
| Autore | Sforza P. M |
| Pubbl/distr/stampa | Waltham, Mass., : Academic Press, c2012 |
| Descrizione fisica | 1 online resource (703 p.) |
| Disciplina | 629.1/1 |
| Collana | Aerospace Engineering |
| Soggetto topico | Jet propulsion |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-283-29364-1
9786613293640 0-12-384889-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Theory of Aerospace Propulsion; Copyright; Contents; Preface; Chapter 1 - Idealized Flow Machines; 1.1 Conservation Equations; 1.2 Flow Machines with No Heat Addition: The Propeller; 1.3 Flow Machines with P = 0 and Q = Constant: The Turbojet, Ramjet, and Scramjet; 1.4 Flow Machines with P = 0, Q = Constant, and A0 = 0: The Rocket; 1.5 The Special Case of Combined Heat and Power: The Turbofan; 1.6 Force Field for Air-Breathing Engines; 1.7 Conditions for Maximum Thrust; 1.8 Example: Jet and Rocket Engine Performance; 1.9 Nomenclature; Reference
Chapter 2 - Quasi-One-Dimensional Flow Equations2.1 Introduction; 2.2 Equation of State; 2.3 Speed of Sound; 2.4 Mach Number; 2.5 Conservation of Mass; 2.6 Conservation of Energy; 2.7 Example: Heating Values for Different Fuel-Oxidizer Combinations; 2.8 Conservation of Species; 2.9 Conservation of Momentum; 2.10 Impulse Function; 2.11 Stagnation Pressure; 2.12 Equations of Motion in Standard Form; 2.13 Example: Flow in a Duct with Friction; 2.14 Nomenclature; References; Chapter 3 - Idealized Cycle Analysis of Jet Propulsion Engines; 3.1 Introduction; 3.2 General Jet Engine Cycle 3.3 Ideal Jet Engine Cycle Analysis3.4 Ideal Turbojet in Maximum Power Take-Off; 3.5 Ideal Turbojet in High Subsonic Cruise in The Stratosphere; 3.6 Ideal Turbojet in Supersonic Cruise in The Stratosphere; 3.7 Ideal Ramjet in High Supersonic Cruise in The Stratosphere; 3.8 Ideal Turbofan in Maximum Power Take-Off; 3.9 Ideal Turbofan in High Subsonic Cruise in The Stratosphere; 3.10 Ideal Internal Turbofan in Supersonic Cruise in The Stratosphere; 3.11 Real Engine Operations; 3.12 Nomenclature; 3.13 Exercises; References; Chapter 4 - Combustion Chambers for Air-Breathing Engines 4.1 Combustion Chamber Attributes4.2 Modeling the Chemical Energy Release; 4.3 Constant Area Combustors; 4.4 Example: Constant Area Combustor; 4.5 Constant Pressure Combustors; 4.6 Fuels for Air-Breathing Engines; 4.7 Combustor Efficiency; 4.8 Combustor Configuration; 4.9 Example: Secondary Air for Cooling; 4.10 Criteria for Equilibrium in Chemical Reactions; 4.11 Calculation of Equilibrium Compositions; 4.12 Example: Homogeneous Reactions with a Direct Solution; 4.13 Example: Homogeneous Reactions with Trial-And-Error Solution 4.14 Example: Estimation of Importance of Neglected Product Species4.15 Adiabatic Flame Temperature; 4.16 Example: Adiabatic Flame Temperature for Stoichiometric H2-O2 Mixture; 4.17 Nomenclature; References; Chapter 5 - Nozzles; 5.1 Nozzle Characteristics and Simplifying Assumptions; 5.2 Flow in a Nozzle with Simple Area Change; 5.3 Mass Flow in an Isentropic Nozzle; 5.4 Nozzle Operation; 5.5 Normal Shock inside the Nozzle; 5.6 Example: Shock in Nozzle; 5.7 Two-Dimensional Considerations in Nozzle Flows; 5.8 Example: Overexpanded Nozzles; 5.9 Example: Underexpanded Nozzles 5.10 Afterburning for Increased Thrust |
| Record Nr. | UNINA-9910457189003321 |
|
Sforza P. M
|
||
| Waltham, Mass., : Academic Press, c2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Theory of aerospace propulsion [[electronic resource] /] / Pasquale M. Sforza
| Theory of aerospace propulsion [[electronic resource] /] / Pasquale M. Sforza |
| Autore | Sforza P. M |
| Pubbl/distr/stampa | Waltham, Mass., : Academic Press, c2012 |
| Descrizione fisica | 1 online resource (703 p.) |
| Disciplina | 629.1/1 |
| Collana | Aerospace Engineering |
| Soggetto topico | Jet propulsion |
| ISBN |
1-283-29364-1
9786613293640 0-12-384889-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Theory of Aerospace Propulsion; Copyright; Contents; Preface; Chapter 1 - Idealized Flow Machines; 1.1 Conservation Equations; 1.2 Flow Machines with No Heat Addition: The Propeller; 1.3 Flow Machines with P = 0 and Q = Constant: The Turbojet, Ramjet, and Scramjet; 1.4 Flow Machines with P = 0, Q = Constant, and A0 = 0: The Rocket; 1.5 The Special Case of Combined Heat and Power: The Turbofan; 1.6 Force Field for Air-Breathing Engines; 1.7 Conditions for Maximum Thrust; 1.8 Example: Jet and Rocket Engine Performance; 1.9 Nomenclature; Reference
Chapter 2 - Quasi-One-Dimensional Flow Equations2.1 Introduction; 2.2 Equation of State; 2.3 Speed of Sound; 2.4 Mach Number; 2.5 Conservation of Mass; 2.6 Conservation of Energy; 2.7 Example: Heating Values for Different Fuel-Oxidizer Combinations; 2.8 Conservation of Species; 2.9 Conservation of Momentum; 2.10 Impulse Function; 2.11 Stagnation Pressure; 2.12 Equations of Motion in Standard Form; 2.13 Example: Flow in a Duct with Friction; 2.14 Nomenclature; References; Chapter 3 - Idealized Cycle Analysis of Jet Propulsion Engines; 3.1 Introduction; 3.2 General Jet Engine Cycle 3.3 Ideal Jet Engine Cycle Analysis3.4 Ideal Turbojet in Maximum Power Take-Off; 3.5 Ideal Turbojet in High Subsonic Cruise in The Stratosphere; 3.6 Ideal Turbojet in Supersonic Cruise in The Stratosphere; 3.7 Ideal Ramjet in High Supersonic Cruise in The Stratosphere; 3.8 Ideal Turbofan in Maximum Power Take-Off; 3.9 Ideal Turbofan in High Subsonic Cruise in The Stratosphere; 3.10 Ideal Internal Turbofan in Supersonic Cruise in The Stratosphere; 3.11 Real Engine Operations; 3.12 Nomenclature; 3.13 Exercises; References; Chapter 4 - Combustion Chambers for Air-Breathing Engines 4.1 Combustion Chamber Attributes4.2 Modeling the Chemical Energy Release; 4.3 Constant Area Combustors; 4.4 Example: Constant Area Combustor; 4.5 Constant Pressure Combustors; 4.6 Fuels for Air-Breathing Engines; 4.7 Combustor Efficiency; 4.8 Combustor Configuration; 4.9 Example: Secondary Air for Cooling; 4.10 Criteria for Equilibrium in Chemical Reactions; 4.11 Calculation of Equilibrium Compositions; 4.12 Example: Homogeneous Reactions with a Direct Solution; 4.13 Example: Homogeneous Reactions with Trial-And-Error Solution 4.14 Example: Estimation of Importance of Neglected Product Species4.15 Adiabatic Flame Temperature; 4.16 Example: Adiabatic Flame Temperature for Stoichiometric H2-O2 Mixture; 4.17 Nomenclature; References; Chapter 5 - Nozzles; 5.1 Nozzle Characteristics and Simplifying Assumptions; 5.2 Flow in a Nozzle with Simple Area Change; 5.3 Mass Flow in an Isentropic Nozzle; 5.4 Nozzle Operation; 5.5 Normal Shock inside the Nozzle; 5.6 Example: Shock in Nozzle; 5.7 Two-Dimensional Considerations in Nozzle Flows; 5.8 Example: Overexpanded Nozzles; 5.9 Example: Underexpanded Nozzles 5.10 Afterburning for Increased Thrust |
| Record Nr. | UNINA-9910781635303321 |
|
Sforza P. M
|
||
| Waltham, Mass., : Academic Press, c2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Theory of aerospace propulsion / / Pasquale M. Sforza
| Theory of aerospace propulsion / / Pasquale M. Sforza |
| Autore | Sforza P. M |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Waltham, Mass., : Academic Press, c2012 |
| Descrizione fisica | 1 online resource (703 p.) |
| Disciplina |
629.1/1
629.11 |
| Collana | Aerospace Engineering |
| Soggetto topico | Jet propulsion |
| ISBN |
1-283-29364-1
9786613293640 0-12-384889-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Theory of Aerospace Propulsion; Copyright; Contents; Preface; Chapter 1 - Idealized Flow Machines; 1.1 Conservation Equations; 1.2 Flow Machines with No Heat Addition: The Propeller; 1.3 Flow Machines with P = 0 and Q = Constant: The Turbojet, Ramjet, and Scramjet; 1.4 Flow Machines with P = 0, Q = Constant, and A0 = 0: The Rocket; 1.5 The Special Case of Combined Heat and Power: The Turbofan; 1.6 Force Field for Air-Breathing Engines; 1.7 Conditions for Maximum Thrust; 1.8 Example: Jet and Rocket Engine Performance; 1.9 Nomenclature; Reference
Chapter 2 - Quasi-One-Dimensional Flow Equations2.1 Introduction; 2.2 Equation of State; 2.3 Speed of Sound; 2.4 Mach Number; 2.5 Conservation of Mass; 2.6 Conservation of Energy; 2.7 Example: Heating Values for Different Fuel-Oxidizer Combinations; 2.8 Conservation of Species; 2.9 Conservation of Momentum; 2.10 Impulse Function; 2.11 Stagnation Pressure; 2.12 Equations of Motion in Standard Form; 2.13 Example: Flow in a Duct with Friction; 2.14 Nomenclature; References; Chapter 3 - Idealized Cycle Analysis of Jet Propulsion Engines; 3.1 Introduction; 3.2 General Jet Engine Cycle 3.3 Ideal Jet Engine Cycle Analysis3.4 Ideal Turbojet in Maximum Power Take-Off; 3.5 Ideal Turbojet in High Subsonic Cruise in The Stratosphere; 3.6 Ideal Turbojet in Supersonic Cruise in The Stratosphere; 3.7 Ideal Ramjet in High Supersonic Cruise in The Stratosphere; 3.8 Ideal Turbofan in Maximum Power Take-Off; 3.9 Ideal Turbofan in High Subsonic Cruise in The Stratosphere; 3.10 Ideal Internal Turbofan in Supersonic Cruise in The Stratosphere; 3.11 Real Engine Operations; 3.12 Nomenclature; 3.13 Exercises; References; Chapter 4 - Combustion Chambers for Air-Breathing Engines 4.1 Combustion Chamber Attributes4.2 Modeling the Chemical Energy Release; 4.3 Constant Area Combustors; 4.4 Example: Constant Area Combustor; 4.5 Constant Pressure Combustors; 4.6 Fuels for Air-Breathing Engines; 4.7 Combustor Efficiency; 4.8 Combustor Configuration; 4.9 Example: Secondary Air for Cooling; 4.10 Criteria for Equilibrium in Chemical Reactions; 4.11 Calculation of Equilibrium Compositions; 4.12 Example: Homogeneous Reactions with a Direct Solution; 4.13 Example: Homogeneous Reactions with Trial-And-Error Solution 4.14 Example: Estimation of Importance of Neglected Product Species4.15 Adiabatic Flame Temperature; 4.16 Example: Adiabatic Flame Temperature for Stoichiometric H2-O2 Mixture; 4.17 Nomenclature; References; Chapter 5 - Nozzles; 5.1 Nozzle Characteristics and Simplifying Assumptions; 5.2 Flow in a Nozzle with Simple Area Change; 5.3 Mass Flow in an Isentropic Nozzle; 5.4 Nozzle Operation; 5.5 Normal Shock inside the Nozzle; 5.6 Example: Shock in Nozzle; 5.7 Two-Dimensional Considerations in Nozzle Flows; 5.8 Example: Overexpanded Nozzles; 5.9 Example: Underexpanded Nozzles 5.10 Afterburning for Increased Thrust |
| Record Nr. | UNINA-9910817660603321 |
|
Sforza P. M
|
||
| Waltham, Mass., : Academic Press, c2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||