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Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi
| Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi |
| Autore | Takahashi Timothy |
| Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
| Descrizione fisica | 1 online resource (xvi, 230 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Aerospace engineering collection |
| Soggetto topico |
Airplanes - Design and construction
Airplanes - Performance |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60650-684-6 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements --
2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes -- 3. Propulsion system design drivers and performance -- 3.1 Gas turbine fundamentals -- 3.2 Calculating thrust and fuel flow -- 3.3 Propulsion system components and design drivers -- 3.4 Example engine performance data -- 4. Aerodynamic analysis fundamentals: lift and drag -- 4.1 Full configuration drag estimation -- 4.2 Zero-lift drag at incompressible speeds -- 4.3 Zero-lift drag due to compressibility -- 4.4 Drag due to lift at incompressible speeds -- 4.5 Drag due to lift arising from compressibility -- 4.6 "Crud drag," the drag of real versus idealized aerostructures -- 4.7 Maximum lift coefficient/buffet boundary -- 4.8 Angle of attack -- 4.9 Take-off, approach, and landing aerodynamics -- 5. Kinematic "point-performance" principles -- 5.1 Standard atmosphere revisited -- 5.2 Computing stall speed -- 5.3 Minimum and maximum permissible flight speeds -- 5.4 The energy-maneuverability skymap plot -- 5.5 Inferring lift and drag in an E-M plot -- 5.6 Aerodynamic efficiency (L/D) and performance efficiency (M(L/D)) -- 5.7 Dimensionalizing drag -- 5.8 Propulsive performance -- 5.9 Specific excess thrust and linear acceleration capability -- 5.10 Specific excess power, rate of climb (R.O.C.), and ceiling -- 5.11 Specific range -- 5.12 Loiter -- 5.13 Induced drag fraction of total drag for level flight limited by aerodynamics and propulsion -- 5.14 Maximum load factor, instantaneous turn rate and stall speed ratio -- 5.15 Combat agility, maximum sustained turn rate -- 6. Mission performance principles -- 6.1 Breguet range equation -- 6.2 Time-step integrating simulations -- 6.3 Creating missions using a mission simulation code -- 6.4 Observations examining the output of a mission simulation code -- 6.5 Creating trade studies using a mission simulation code -- 6.6 Creating payload/range charts using a mission simulation code -- Index. |
| Record Nr. | UNINA-9910465946303321 |
Takahashi Timothy
|
||
| New York, NY : , : Momentum Press, , [2018] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi
| Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi |
| Autore | Takahashi Timothy |
| Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
| Descrizione fisica | 1 online resource (xvi, 230 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Aerospace engineering collection |
| Soggetto topico |
Airplanes - Design and construction
Airplanes - Performance |
| ISBN | 1-60650-684-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements --
2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes -- 3. Propulsion system design drivers and performance -- 3.1 Gas turbine fundamentals -- 3.2 Calculating thrust and fuel flow -- 3.3 Propulsion system components and design drivers -- 3.4 Example engine performance data -- 4. Aerodynamic analysis fundamentals: lift and drag -- 4.1 Full configuration drag estimation -- 4.2 Zero-lift drag at incompressible speeds -- 4.3 Zero-lift drag due to compressibility -- 4.4 Drag due to lift at incompressible speeds -- 4.5 Drag due to lift arising from compressibility -- 4.6 "Crud drag," the drag of real versus idealized aerostructures -- 4.7 Maximum lift coefficient/buffet boundary -- 4.8 Angle of attack -- 4.9 Take-off, approach, and landing aerodynamics -- 5. Kinematic "point-performance" principles -- 5.1 Standard atmosphere revisited -- 5.2 Computing stall speed -- 5.3 Minimum and maximum permissible flight speeds -- 5.4 The energy-maneuverability skymap plot -- 5.5 Inferring lift and drag in an E-M plot -- 5.6 Aerodynamic efficiency (L/D) and performance efficiency (M(L/D)) -- 5.7 Dimensionalizing drag -- 5.8 Propulsive performance -- 5.9 Specific excess thrust and linear acceleration capability -- 5.10 Specific excess power, rate of climb (R.O.C.), and ceiling -- 5.11 Specific range -- 5.12 Loiter -- 5.13 Induced drag fraction of total drag for level flight limited by aerodynamics and propulsion -- 5.14 Maximum load factor, instantaneous turn rate and stall speed ratio -- 5.15 Combat agility, maximum sustained turn rate -- 6. Mission performance principles -- 6.1 Breguet range equation -- 6.2 Time-step integrating simulations -- 6.3 Creating missions using a mission simulation code -- 6.4 Observations examining the output of a mission simulation code -- 6.5 Creating trade studies using a mission simulation code -- 6.6 Creating payload/range charts using a mission simulation code -- Index. |
| Record Nr. | UNINA-9910798269903321 |
|
Takahashi Timothy
|
||
| New York, NY : , : Momentum Press, , [2018] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft performance and sizing . Volume II : applied aerodynamic design / / Timothy Takahashi
| Aircraft performance and sizing . Volume II : applied aerodynamic design / / Timothy Takahashi |
| Autore | Takahashi Timothy |
| Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
| Descrizione fisica | 1 online resource (xvii, 250 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Aerospace engineering collection |
| Soggetto topico | Airplanes - Design and construction |
| ISBN | 1-60650-946-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
1. Systems engineering and the design process -- 1.1 The systems engineering vee, a plan for success -- 1.2 Conceptual design -- 1.3 Multidisciplinary trade studies -- 1.4 Model fidelity -- 1.5 Detail design -- 1.6 Risk reduction and mitigation --
2. Weight and volume estimation -- 2.1 A self referential problem: how much an aircraft weighs at takeoff is a function of how much it weighs empty -- 2.2 Approaches to aircraft sizing -- 2.3 Empirical methods to estimate empty weight -- 2.4 Modeling and simulation methods to estimate empty weight -- 2.5 Estimating mass moments of inertia -- 3. Stability and controllability -- 3.1 Aerodynamic database generation -- 3.2 Aerodynamic database presentation -- 3.3 Empirical methods to size the vertical and horizontal tail -- 3.4 Modeling and simulation approach to stability and control -- 3.5 Longitudinal trim -- 3.6 Longitudinal stability -- 3.7 CG placement, horizontal tail, and elevator sizing -- 3.8 Lateral-directional trim -- 3.9 Lateral-directional stability -- 3.10 Lateral-directional control -- 4. Field performance principles -- 4.1 Takeoff in a nutshell -- 4.2 Simplified statistical method for takeoff -- 4.3 Computing takeoff cue speeds -- 4.4 Modeling and simulation methods for takeoff -- 4.5 Takeoff noise, certification and abatement procedures -- 4.6 Approach and landing in a nutshell -- 4.7 Computing landing cue speeds -- 4.8 Simplified statistical model for landing -- 4.9 Modeling and simulation methods for landing -- 5. The aerodynamic design of wings -- 5.1 Planform geometry -- 5.2 Three-dimensional flow effects -- 5.3 Transonic flow over two-dimensional airfoils -- 5.4 Selecting an appropriate airfoil for transonic flight -- 5.5 Sweep effects -- 5.6 Nonplanarity -- 5.7 Designing a wing for optimal performance -- 6. Aircraft sizing and synthesis, putting it all together -- 6.1 Aircraft sizing in a nutshell -- 6.2 Simple sizing using Breguet's equation -- 6.3 Sizing using a multidisciplinary optimization approach -- 6.4 Systems design examples -- 6.5 Afterword -- Index. |
| Record Nr. | UNINA-9910798265703321 |
|
Takahashi Timothy
|
||
| New York, NY : , : Momentum Press, , [2018] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi
| Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi |
| Autore | Takahashi Timothy |
| Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
| Descrizione fisica | 1 online resource (xvi, 230 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Aerospace engineering collection |
| Soggetto topico |
Airplanes - Design and construction
Airplanes - Performance |
| ISBN | 1-60650-684-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements --
2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes -- 3. Propulsion system design drivers and performance -- 3.1 Gas turbine fundamentals -- 3.2 Calculating thrust and fuel flow -- 3.3 Propulsion system components and design drivers -- 3.4 Example engine performance data -- 4. Aerodynamic analysis fundamentals: lift and drag -- 4.1 Full configuration drag estimation -- 4.2 Zero-lift drag at incompressible speeds -- 4.3 Zero-lift drag due to compressibility -- 4.4 Drag due to lift at incompressible speeds -- 4.5 Drag due to lift arising from compressibility -- 4.6 "Crud drag," the drag of real versus idealized aerostructures -- 4.7 Maximum lift coefficient/buffet boundary -- 4.8 Angle of attack -- 4.9 Take-off, approach, and landing aerodynamics -- 5. Kinematic "point-performance" principles -- 5.1 Standard atmosphere revisited -- 5.2 Computing stall speed -- 5.3 Minimum and maximum permissible flight speeds -- 5.4 The energy-maneuverability skymap plot -- 5.5 Inferring lift and drag in an E-M plot -- 5.6 Aerodynamic efficiency (L/D) and performance efficiency (M(L/D)) -- 5.7 Dimensionalizing drag -- 5.8 Propulsive performance -- 5.9 Specific excess thrust and linear acceleration capability -- 5.10 Specific excess power, rate of climb (R.O.C.), and ceiling -- 5.11 Specific range -- 5.12 Loiter -- 5.13 Induced drag fraction of total drag for level flight limited by aerodynamics and propulsion -- 5.14 Maximum load factor, instantaneous turn rate and stall speed ratio -- 5.15 Combat agility, maximum sustained turn rate -- 6. Mission performance principles -- 6.1 Breguet range equation -- 6.2 Time-step integrating simulations -- 6.3 Creating missions using a mission simulation code -- 6.4 Observations examining the output of a mission simulation code -- 6.5 Creating trade studies using a mission simulation code -- 6.6 Creating payload/range charts using a mission simulation code -- Index. |
| Record Nr. | UNINA-9910816426203321 |
|
Takahashi Timothy
|
||
| New York, NY : , : Momentum Press, , [2018] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft performance and sizing . Volume II : applied aerodynamic design / / Timothy Takahashi
| Aircraft performance and sizing . Volume II : applied aerodynamic design / / Timothy Takahashi |
| Autore | Takahashi Timothy |
| Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
| Descrizione fisica | 1 online resource (xvii, 250 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Aerospace engineering collection |
| Soggetto topico | Airplanes - Design and construction |
| ISBN | 1-60650-946-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
1. Systems engineering and the design process -- 1.1 The systems engineering vee, a plan for success -- 1.2 Conceptual design -- 1.3 Multidisciplinary trade studies -- 1.4 Model fidelity -- 1.5 Detail design -- 1.6 Risk reduction and mitigation --
2. Weight and volume estimation -- 2.1 A self referential problem: how much an aircraft weighs at takeoff is a function of how much it weighs empty -- 2.2 Approaches to aircraft sizing -- 2.3 Empirical methods to estimate empty weight -- 2.4 Modeling and simulation methods to estimate empty weight -- 2.5 Estimating mass moments of inertia -- 3. Stability and controllability -- 3.1 Aerodynamic database generation -- 3.2 Aerodynamic database presentation -- 3.3 Empirical methods to size the vertical and horizontal tail -- 3.4 Modeling and simulation approach to stability and control -- 3.5 Longitudinal trim -- 3.6 Longitudinal stability -- 3.7 CG placement, horizontal tail, and elevator sizing -- 3.8 Lateral-directional trim -- 3.9 Lateral-directional stability -- 3.10 Lateral-directional control -- 4. Field performance principles -- 4.1 Takeoff in a nutshell -- 4.2 Simplified statistical method for takeoff -- 4.3 Computing takeoff cue speeds -- 4.4 Modeling and simulation methods for takeoff -- 4.5 Takeoff noise, certification and abatement procedures -- 4.6 Approach and landing in a nutshell -- 4.7 Computing landing cue speeds -- 4.8 Simplified statistical model for landing -- 4.9 Modeling and simulation methods for landing -- 5. The aerodynamic design of wings -- 5.1 Planform geometry -- 5.2 Three-dimensional flow effects -- 5.3 Transonic flow over two-dimensional airfoils -- 5.4 Selecting an appropriate airfoil for transonic flight -- 5.5 Sweep effects -- 5.6 Nonplanarity -- 5.7 Designing a wing for optimal performance -- 6. Aircraft sizing and synthesis, putting it all together -- 6.1 Aircraft sizing in a nutshell -- 6.2 Simple sizing using Breguet's equation -- 6.3 Sizing using a multidisciplinary optimization approach -- 6.4 Systems design examples -- 6.5 Afterword -- Index. |
| Record Nr. | UNINA-9910809930403321 |
|
Takahashi Timothy
|
||
| New York, NY : , : Momentum Press, , [2018] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aricraft performance and sizing . Volume II : applied aerodynamic design / / Timothy Takahashi
| Aricraft performance and sizing . Volume II : applied aerodynamic design / / Timothy Takahashi |
| Autore | Takahashi Timothy |
| Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
| Descrizione fisica | 1 online resource (xvii, 250 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Aerospace engineering collection |
| Soggetto topico | Airplanes - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60650-946-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
1. Systems engineering and the design process -- 1.1 The systems engineering vee, a plan for success -- 1.2 Conceptual design -- 1.3 Multidisciplinary trade studies -- 1.4 Model fidelity -- 1.5 Detail design -- 1.6 Risk reduction and mitigation --
2. Weight and volume estimation -- 2.1 A self referential problem: how much an aircraft weighs at takeoff is a function of how much it weighs empty -- 2.2 Approaches to aircraft sizing -- 2.3 Empirical methods to estimate empty weight -- 2.4 Modeling and simulation methods to estimate empty weight -- 2.5 Estimating mass moments of inertia -- 3. Stability and controllability -- 3.1 Aerodynamic database generation -- 3.2 Aerodynamic database presentation -- 3.3 Empirical methods to size the vertical and horizontal tail -- 3.4 Modeling and simulation approach to stability and control -- 3.5 Longitudinal trim -- 3.6 Longitudinal stability -- 3.7 CG placement, horizontal tail, and elevator sizing -- 3.8 Lateral-directional trim -- 3.9 Lateral-directional stability -- 3.10 Lateral-directional control -- 4. Field performance principles -- 4.1 Takeoff in a nutshell -- 4.2 Simplified statistical method for takeoff -- 4.3 Computing takeoff cue speeds -- 4.4 Modeling and simulation methods for takeoff -- 4.5 Takeoff noise, certification and abatement procedures -- 4.6 Approach and landing in a nutshell -- 4.7 Computing landing cue speeds -- 4.8 Simplified statistical model for landing -- 4.9 Modeling and simulation methods for landing -- 5. The aerodynamic design of wings -- 5.1 Planform geometry -- 5.2 Three-dimensional flow effects -- 5.3 Transonic flow over two-dimensional airfoils -- 5.4 Selecting an appropriate airfoil for transonic flight -- 5.5 Sweep effects -- 5.6 Nonplanarity -- 5.7 Designing a wing for optimal performance -- 6. Aircraft sizing and synthesis, putting it all together -- 6.1 Aircraft sizing in a nutshell -- 6.2 Simple sizing using Breguet's equation -- 6.3 Sizing using a multidisciplinary optimization approach -- 6.4 Systems design examples -- 6.5 Afterword -- Index. |
| Record Nr. | UNINA-9910465946603321 |
|
Takahashi Timothy
|
||
| New York, NY : , : Momentum Press, , [2018] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||