Energy and motorization in the automotive and aeronautics industries / / Tomasz Krysinski, Francois Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London, UK ; ; Hoboken, NJ : , : ISTE Ltd. : , : Wiley, , 2020 |
Descrizione fisica | 1 online resource (330 pages) |
Disciplina | 658.406 |
Soggetto topico |
Automobile industry and trade - Technological innovations
Aerospace industries - Technological innovations |
Soggetto genere / forma | Electronic books. |
ISBN |
1-119-77702-X
1-5231-3678-2 1-119-77704-6 1-119-77703-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910555175503321 |
Krysinski Tomasz
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||
London, UK ; ; Hoboken, NJ : , : ISTE Ltd. : , : Wiley, , 2020 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|
Energy and motorization in the automotive and aeronautics industries / / Tomasz Krysinski, Francois Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London, UK ; ; Hoboken, NJ : , : ISTE Ltd. : , : Wiley, , 2020 |
Descrizione fisica | 1 online resource (330 pages) |
Disciplina | 658.406 |
Soggetto topico |
Automobile industry and trade - Technological innovations
Aerospace industries - Technological innovations |
ISBN |
1-119-77702-X
1-5231-3678-2 1-119-77704-6 1-119-77703-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910829974303321 |
Krysinski Tomasz
![]() |
||
London, UK ; ; Hoboken, NJ : , : ISTE Ltd. : , : Wiley, , 2020 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
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Mechanical instability [[electronic resource] /] / Tomasz Krysinski, François Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London, U.K., : ISTE |
Descrizione fisica | 1 online resource (368 p.) |
Disciplina | 620.1 |
Altri autori (Persone) | MalburetFrançois |
Collana | ISTE |
Soggetto topico |
Dynamics
Mechanics, Applied Mechanical engineering Stability Vibration |
ISBN |
1-118-60084-3
1-118-60095-9 1-118-60077-0 1-299-18748-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Notions of instability -- Rotor-structure coupling : ground resonance and air resonance examples -- Chain torsion : instability of feedback systems -- Self-exited vibrations -- Fluid-structure interaction. |
Record Nr. | UNINA-9910138853103321 |
Krysinski Tomasz
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||
London, U.K., : ISTE | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
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Mechanical instability / / Tomasz Krysinski, François Malburet |
Autore | Krysinski Tomasz |
Edizione | [1st ed.] |
Pubbl/distr/stampa | London, U.K., : ISTE |
Descrizione fisica | 1 online resource (368 p.) |
Disciplina | 620.1 |
Altri autori (Persone) | MalburetFrançois |
Collana | ISTE |
Soggetto topico |
Dynamics
Mechanics, Applied Mechanical engineering Stability Vibration |
ISBN |
1-118-60084-3
1-118-60095-9 1-118-60077-0 1-299-18748-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Notions of instability -- Rotor-structure coupling : ground resonance and air resonance examples -- Chain torsion : instability of feedback systems -- Self-exited vibrations -- Fluid-structure interaction. |
Record Nr. | UNINA-9910814081103321 |
Krysinski Tomasz
![]() |
||
London, U.K., : ISTE | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|
Mechanical vibrations [[electronic resource] ] : active and passive control / / Tomasz Krysinski, François Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London ; ; Newport Beach, CA, : ISTE, c2007 |
Descrizione fisica | 1 online resource (391 p.) |
Disciplina |
620.3
621.8/11 621.811 |
Altri autori (Persone) | MalburetFrançois |
Collana | ISTE |
Soggetto topico |
Rotors - Vibration
Damping (Mechanics) Structural control (Engineering) |
Soggetto genere / forma | Electronic books. |
ISBN |
1-280-84767-0
9786610847679 0-470-61247-9 0-470-39460-9 1-84704-579-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Mechanical Vibrations; Table of Contents; Foreword; Preface; Part I. Sources of Vibrations; Chapter 1. Unbalance and Gyroscopic Effects; 1.1. Introduction; 1.1.1. Physico-mathematical model of a rotating system; 1.1.2. Formation of equations and analysis; 1.2. Theory of balancing; 1.2.1. Balancing machine or "balancer"; 1.2.1.1. The soft-bearing machine; 1.2.1.2. The hard-bearing machine; 1.2.2. Balancing in situ; 1.2.2.1. The method of separate planes; 1.2.2.2. The method of simultaneous planes - influence coefficients; 1.2.3. Example of application: the main rotor of a helicopter
1.2.3.1. Bench test phase on the ground1.2.3.2. Test phase on a helicopter in flight; 1.3. Influence of shaft bending; 1.3.1. The notion of critical speed; 1.3.2. Forward precession of the flexible shaft; 1.3.2.1. Subcritical speed (: Ω<ωcr); 1.3.2.2. Resonance (: Ω<ωcr); 1.3.2.3. Supercritical speed (: Ω<ωcr); 1.3.3. Balancing flexible shafts; 1.3.4. Example of application: transmission shaft of the tail rotor of a helicopter; 1.4. Gyroscopic effects; 1.4.1. Forward or backward motion; 1.4.2. Equations of motion; 1.4.2.1. Natural angular frequencies (shaft off motion) 1.4.2.2. Critical speeds during forward precession1.4.2.3. Critical speeds during retrograde precession; Chapter 2. Piston Engines; 2.1. Introduction; 2.2. Excitations generated by a piston engine; 2.2.1. Analytic determination of an engine torque; 2.2.2. Engine excitations on the chassis frame; 2.2.2.1. Knocking load; 2.2.2.2. Pitch torque; 2.2.2.3. Review of actions for a four phase cylinder engine; 2.2.3. The notion of engine balancing; 2.2.3.1. Balancing the knocking loads; 2.2.3.2. Balancing the galloping torque; 2.3. Line shafting tuning; 2.3.1. The notion of tuning 2.3.2. Creation of the equations2.3.3. Line shafting optimization; 2.3.3.1. Results for a non-optimized line shafting; 2.3.3.2. Results for an optimized line shafting; Chapter 3. Dynamics of a Rotor; 3.1. Introduction; 3.2. Description of the blade/hub relationship; 3.2.1. Some historical data; 3.2.2. Hinge link of the blade and the hub; 3.2.2.1. Formation of the equations for blade motion; 3.2.2.2. Homokinetic rotor; 3.3. Rotor technologies; 3.3.1. Articulated rotors; 3.3.1.1. Conventional articulated rotors; 3.3.1.2. Starflex® and Spheriflex® rotors; 3.3.2. Hingeless rotors 3.3.3. Hingeless rotor3.4. Influence of alternate aerodynamic loads; 3.4.1. Load characterization; 3.4.1.1. Loads on a blade; 3.4.1.2. Dynamic response of a blade; 3.4.1.3. Loads transmitted by a mode i; 3.4.2. Analysis of loads transmitted to the rotor hub; 3.4.2.1. Loads transmitted to the rotor; 3.4.2.2. Synthesis of rotor loads on the rotor mast; 3.4.3. Dynamic optimization of a blade; 3.4.3.1. Introduction; 3.4.3.2. Study of the example of an optimized blade; 3.4.3.3. Contribution of the second flapping mode; Chapter 4. Rotor Control; 4.1. Introduction; 4.2. Blade motions 4.2.1. Flapping equation - general case |
Record Nr. | UNINA-9910143315003321 |
Krysinski Tomasz
![]() |
||
London ; ; Newport Beach, CA, : ISTE, c2007 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|
Mechanical vibrations [[electronic resource] ] : active and passive control / / Tomasz Krysinski, François Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London ; ; Newport Beach, CA, : ISTE, c2007 |
Descrizione fisica | 1 online resource (391 p.) |
Disciplina |
620.3
621.8/11 621.811 |
Altri autori (Persone) | MalburetFrançois |
Collana | ISTE |
Soggetto topico |
Rotors - Vibration
Damping (Mechanics) Structural control (Engineering) |
ISBN |
1-280-84767-0
9786610847679 0-470-61247-9 0-470-39460-9 1-84704-579-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Mechanical Vibrations; Table of Contents; Foreword; Preface; Part I. Sources of Vibrations; Chapter 1. Unbalance and Gyroscopic Effects; 1.1. Introduction; 1.1.1. Physico-mathematical model of a rotating system; 1.1.2. Formation of equations and analysis; 1.2. Theory of balancing; 1.2.1. Balancing machine or "balancer"; 1.2.1.1. The soft-bearing machine; 1.2.1.2. The hard-bearing machine; 1.2.2. Balancing in situ; 1.2.2.1. The method of separate planes; 1.2.2.2. The method of simultaneous planes - influence coefficients; 1.2.3. Example of application: the main rotor of a helicopter
1.2.3.1. Bench test phase on the ground1.2.3.2. Test phase on a helicopter in flight; 1.3. Influence of shaft bending; 1.3.1. The notion of critical speed; 1.3.2. Forward precession of the flexible shaft; 1.3.2.1. Subcritical speed (: Ω<ωcr); 1.3.2.2. Resonance (: Ω<ωcr); 1.3.2.3. Supercritical speed (: Ω<ωcr); 1.3.3. Balancing flexible shafts; 1.3.4. Example of application: transmission shaft of the tail rotor of a helicopter; 1.4. Gyroscopic effects; 1.4.1. Forward or backward motion; 1.4.2. Equations of motion; 1.4.2.1. Natural angular frequencies (shaft off motion) 1.4.2.2. Critical speeds during forward precession1.4.2.3. Critical speeds during retrograde precession; Chapter 2. Piston Engines; 2.1. Introduction; 2.2. Excitations generated by a piston engine; 2.2.1. Analytic determination of an engine torque; 2.2.2. Engine excitations on the chassis frame; 2.2.2.1. Knocking load; 2.2.2.2. Pitch torque; 2.2.2.3. Review of actions for a four phase cylinder engine; 2.2.3. The notion of engine balancing; 2.2.3.1. Balancing the knocking loads; 2.2.3.2. Balancing the galloping torque; 2.3. Line shafting tuning; 2.3.1. The notion of tuning 2.3.2. Creation of the equations2.3.3. Line shafting optimization; 2.3.3.1. Results for a non-optimized line shafting; 2.3.3.2. Results for an optimized line shafting; Chapter 3. Dynamics of a Rotor; 3.1. Introduction; 3.2. Description of the blade/hub relationship; 3.2.1. Some historical data; 3.2.2. Hinge link of the blade and the hub; 3.2.2.1. Formation of the equations for blade motion; 3.2.2.2. Homokinetic rotor; 3.3. Rotor technologies; 3.3.1. Articulated rotors; 3.3.1.1. Conventional articulated rotors; 3.3.1.2. Starflex® and Spheriflex® rotors; 3.3.2. Hingeless rotors 3.3.3. Hingeless rotor3.4. Influence of alternate aerodynamic loads; 3.4.1. Load characterization; 3.4.1.1. Loads on a blade; 3.4.1.2. Dynamic response of a blade; 3.4.1.3. Loads transmitted by a mode i; 3.4.2. Analysis of loads transmitted to the rotor hub; 3.4.2.1. Loads transmitted to the rotor; 3.4.2.2. Synthesis of rotor loads on the rotor mast; 3.4.3. Dynamic optimization of a blade; 3.4.3.1. Introduction; 3.4.3.2. Study of the example of an optimized blade; 3.4.3.3. Contribution of the second flapping mode; Chapter 4. Rotor Control; 4.1. Introduction; 4.2. Blade motions 4.2.1. Flapping equation - general case |
Record Nr. | UNISA-996216941603316 |
Krysinski Tomasz
![]() |
||
London ; ; Newport Beach, CA, : ISTE, c2007 | ||
![]() | ||
Lo trovi qui: Univ. di Salerno | ||
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Mechanical vibrations [[electronic resource] ] : active and passive control / / Tomasz Krysinski, François Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London ; ; Newport Beach, CA, : ISTE, c2007 |
Descrizione fisica | 1 online resource (391 p.) |
Disciplina |
620.3
621.8/11 621.811 |
Altri autori (Persone) | MalburetFrançois |
Collana | ISTE |
Soggetto topico |
Rotors - Vibration
Damping (Mechanics) Structural control (Engineering) |
ISBN |
1-280-84767-0
9786610847679 0-470-61247-9 0-470-39460-9 1-84704-579-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Mechanical Vibrations; Table of Contents; Foreword; Preface; Part I. Sources of Vibrations; Chapter 1. Unbalance and Gyroscopic Effects; 1.1. Introduction; 1.1.1. Physico-mathematical model of a rotating system; 1.1.2. Formation of equations and analysis; 1.2. Theory of balancing; 1.2.1. Balancing machine or "balancer"; 1.2.1.1. The soft-bearing machine; 1.2.1.2. The hard-bearing machine; 1.2.2. Balancing in situ; 1.2.2.1. The method of separate planes; 1.2.2.2. The method of simultaneous planes - influence coefficients; 1.2.3. Example of application: the main rotor of a helicopter
1.2.3.1. Bench test phase on the ground1.2.3.2. Test phase on a helicopter in flight; 1.3. Influence of shaft bending; 1.3.1. The notion of critical speed; 1.3.2. Forward precession of the flexible shaft; 1.3.2.1. Subcritical speed (: Ω<ωcr); 1.3.2.2. Resonance (: Ω<ωcr); 1.3.2.3. Supercritical speed (: Ω<ωcr); 1.3.3. Balancing flexible shafts; 1.3.4. Example of application: transmission shaft of the tail rotor of a helicopter; 1.4. Gyroscopic effects; 1.4.1. Forward or backward motion; 1.4.2. Equations of motion; 1.4.2.1. Natural angular frequencies (shaft off motion) 1.4.2.2. Critical speeds during forward precession1.4.2.3. Critical speeds during retrograde precession; Chapter 2. Piston Engines; 2.1. Introduction; 2.2. Excitations generated by a piston engine; 2.2.1. Analytic determination of an engine torque; 2.2.2. Engine excitations on the chassis frame; 2.2.2.1. Knocking load; 2.2.2.2. Pitch torque; 2.2.2.3. Review of actions for a four phase cylinder engine; 2.2.3. The notion of engine balancing; 2.2.3.1. Balancing the knocking loads; 2.2.3.2. Balancing the galloping torque; 2.3. Line shafting tuning; 2.3.1. The notion of tuning 2.3.2. Creation of the equations2.3.3. Line shafting optimization; 2.3.3.1. Results for a non-optimized line shafting; 2.3.3.2. Results for an optimized line shafting; Chapter 3. Dynamics of a Rotor; 3.1. Introduction; 3.2. Description of the blade/hub relationship; 3.2.1. Some historical data; 3.2.2. Hinge link of the blade and the hub; 3.2.2.1. Formation of the equations for blade motion; 3.2.2.2. Homokinetic rotor; 3.3. Rotor technologies; 3.3.1. Articulated rotors; 3.3.1.1. Conventional articulated rotors; 3.3.1.2. Starflex® and Spheriflex® rotors; 3.3.2. Hingeless rotors 3.3.3. Hingeless rotor3.4. Influence of alternate aerodynamic loads; 3.4.1. Load characterization; 3.4.1.1. Loads on a blade; 3.4.1.2. Dynamic response of a blade; 3.4.1.3. Loads transmitted by a mode i; 3.4.2. Analysis of loads transmitted to the rotor hub; 3.4.2.1. Loads transmitted to the rotor; 3.4.2.2. Synthesis of rotor loads on the rotor mast; 3.4.3. Dynamic optimization of a blade; 3.4.3.1. Introduction; 3.4.3.2. Study of the example of an optimized blade; 3.4.3.3. Contribution of the second flapping mode; Chapter 4. Rotor Control; 4.1. Introduction; 4.2. Blade motions 4.2.1. Flapping equation - general case |
Record Nr. | UNINA-9910830101203321 |
Krysinski Tomasz
![]() |
||
London ; ; Newport Beach, CA, : ISTE, c2007 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|
Mechanical vibrations : active and passive control / / Tomasz Krysinski, Francois Malburet |
Autore | Krysinski Tomasz |
Pubbl/distr/stampa | London ; ; Newport Beach, CA, : ISTE, c2007 |
Descrizione fisica | 1 online resource (391 p.) |
Disciplina | 621.8/11 |
Altri autori (Persone) | MalburetFrancois |
Collana | ISTE |
Soggetto topico |
Rotors - Vibration
Damping (Mechanics) Structural control (Engineering) |
ISBN |
1-280-84767-0
9786610847679 0-470-61247-9 0-470-39460-9 1-84704-579-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Mechanical Vibrations; Table of Contents; Foreword; Preface; Part I. Sources of Vibrations; Chapter 1. Unbalance and Gyroscopic Effects; 1.1. Introduction; 1.1.1. Physico-mathematical model of a rotating system; 1.1.2. Formation of equations and analysis; 1.2. Theory of balancing; 1.2.1. Balancing machine or "balancer"; 1.2.1.1. The soft-bearing machine; 1.2.1.2. The hard-bearing machine; 1.2.2. Balancing in situ; 1.2.2.1. The method of separate planes; 1.2.2.2. The method of simultaneous planes - influence coefficients; 1.2.3. Example of application: the main rotor of a helicopter
1.2.3.1. Bench test phase on the ground1.2.3.2. Test phase on a helicopter in flight; 1.3. Influence of shaft bending; 1.3.1. The notion of critical speed; 1.3.2. Forward precession of the flexible shaft; 1.3.2.1. Subcritical speed (: Ω<ωcr); 1.3.2.2. Resonance (: Ω<ωcr); 1.3.2.3. Supercritical speed (: Ω<ωcr); 1.3.3. Balancing flexible shafts; 1.3.4. Example of application: transmission shaft of the tail rotor of a helicopter; 1.4. Gyroscopic effects; 1.4.1. Forward or backward motion; 1.4.2. Equations of motion; 1.4.2.1. Natural angular frequencies (shaft off motion) 1.4.2.2. Critical speeds during forward precession1.4.2.3. Critical speeds during retrograde precession; Chapter 2. Piston Engines; 2.1. Introduction; 2.2. Excitations generated by a piston engine; 2.2.1. Analytic determination of an engine torque; 2.2.2. Engine excitations on the chassis frame; 2.2.2.1. Knocking load; 2.2.2.2. Pitch torque; 2.2.2.3. Review of actions for a four phase cylinder engine; 2.2.3. The notion of engine balancing; 2.2.3.1. Balancing the knocking loads; 2.2.3.2. Balancing the galloping torque; 2.3. Line shafting tuning; 2.3.1. The notion of tuning 2.3.2. Creation of the equations2.3.3. Line shafting optimization; 2.3.3.1. Results for a non-optimized line shafting; 2.3.3.2. Results for an optimized line shafting; Chapter 3. Dynamics of a Rotor; 3.1. Introduction; 3.2. Description of the blade/hub relationship; 3.2.1. Some historical data; 3.2.2. Hinge link of the blade and the hub; 3.2.2.1. Formation of the equations for blade motion; 3.2.2.2. Homokinetic rotor; 3.3. Rotor technologies; 3.3.1. Articulated rotors; 3.3.1.1. Conventional articulated rotors; 3.3.1.2. Starflex® and Spheriflex® rotors; 3.3.2. Hingeless rotors 3.3.3. Hingeless rotor3.4. Influence of alternate aerodynamic loads; 3.4.1. Load characterization; 3.4.1.1. Loads on a blade; 3.4.1.2. Dynamic response of a blade; 3.4.1.3. Loads transmitted by a mode i; 3.4.2. Analysis of loads transmitted to the rotor hub; 3.4.2.1. Loads transmitted to the rotor; 3.4.2.2. Synthesis of rotor loads on the rotor mast; 3.4.3. Dynamic optimization of a blade; 3.4.3.1. Introduction; 3.4.3.2. Study of the example of an optimized blade; 3.4.3.3. Contribution of the second flapping mode; Chapter 4. Rotor Control; 4.1. Introduction; 4.2. Blade motions 4.2.1. Flapping equation - general case |
Record Nr. | UNINA-9910876693903321 |
Krysinski Tomasz
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||
London ; ; Newport Beach, CA, : ISTE, c2007 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
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