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Aircraft dynamic stability and response / / A. W. Babister
| Aircraft dynamic stability and response / / A. W. Babister |
| Autore | Babister A. W. |
| Edizione | [First edition.] |
| Pubbl/distr/stampa | Oxford, England : , : Pergamon Press, , 1986 |
| Descrizione fisica | 1 online resource (247 p.) |
| Disciplina | 629.13236 |
| Collana | Pergamon International Library of Science, Technology, Engineering and Social Studies |
| Soggetto topico |
Stability of airplanes
Airplanes - Handling characteristics |
| ISBN | 1-4831-4035-0 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Dynamic Stability and Response; Copyright Page; Table of Contents; Preface; List Of Symbols; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; UNITS; Part I: FLIGHT DYNAMICS; Chapter 1.INTRODUCTION; THE GENERAL MEANING OF STABILITY; LONGITUDINAL STATIC STABILITY; STATIC MARGIN; STABILITY AND TRIM; MANOEUVRABILITY AND MANOEUVRE MARGIN; REFERENCES; PROBLEMS; Chapter 2. THE EQUATIONS OF MOTION; INTRODUCTION; THE GENERAL DYNAMICAL EQUATIONS FOR A RIGID AIRCRAFT REFERRED TO MOVING AXES
DEFINITION OF THE ANGLE OF PITCH θ, THE ANGLE OF BANK Φ AND ANGLE OF YAW ψRELATIONS FOR RATES OF ROLL, PITCH AND YAW; DETERMINATION OF THE GRAVITATIONAL FORCES; ANGLES OF YAW AND SIDESLIP; DETERMINATION OF THE AERODYNAMIC FORCES; SEPARABILITY OF LONGITUDINAL AND LATERAL MOTION; AXIS SYSTEMS USED IN STABILITY ANALYSIS; NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LONGITUDINAL); NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LATERAL); NON-DIMENSIONAL DISTURBANCES; NON-DIMENSIONAL MASS AND INERTIA; NON-DIMENSIONAL FORM OF THE EQUATIONS OF MOTION; THE MOTION OF THE CENTRE OF GRAVITY OF THE AIRCRAFT REFERENCESPROBLEMS; Chapter 3. AERODYNAMIC DERIVATIVES (LONGITUDINAL); INTRODUCTION; FORCE VELOCITY DERIVATIVES Xu, Xw, Zu, Zw; INCIDENCE CHANGE ASSOCIATED WITH CHANGE IN VELOCITY COMPONENTS; PITCHING MOMENT DERIVATIVES Mu, Mw; DERIVATIVES DUE TO RATE OF PITCH Xq, Zq, Mq; DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY X'w, Z'w, M'w; CONTROL DERIVATIVES; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; AMERICAN NON-DIMENSIONAL FORCE-VELOCITY DERIVATIVES cxu, cxα, czu, czα,; AMERICAN NON-DIMENSIONAL PITCHING MOMENT DERIVATIVES Cmu, Cma AMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF PITCH cxq, czq, cmqAMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY CxDα, CzDα, CmDα; AMERICAN NON-DIMENSIONAL CONTROL DERIVATIVES Cxδe, CZδe, Cmδe DUE TO ELEVATOR; REFERENCES; PROBLEMS; Chapter 4. AERODYNAMIC DERIVATIVES (LATERAL); INTRODUCTION; ESTIMATION OF LATERAL STABILITY DERIVATIVES; DERIVATIVES DUE TO SIDESLIP; DERIVATIVES DUE TO RATE OF ROLL; DERIVATIVES DUE TO RATE OF YAW; CONTROL DERIVATIVES; DERIVATIVES DUE TO AILERONS; DERIVATIVES DUE TO RUDDER NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICANON-DIMENSIONAL FORMS OF THE CONTROL DERIVATIVES USED IN AMERICA; REFERENCES; PROBLEMS; Part II: LONGITUDINAL DYNAMIC STABILITY AND RESPONSE; Chapter 5. BASIC LONGITUDINAL MOTIONS; INTRODUCTION; THE SHORT PERIOD OSCILLATION; THE PHUGOID (LONG PERIOD) OSCILLATION; PROBLEMS; Chapter 6. LONGITUDINAL DYNAMIC STABILITY; INTRODUCTION; STICK FIXED DYNAMIC STABILITY; THE GENERAL SOLUTION OF THE EQUATIONS OF MOTION; TYPES OF MOTION CORRESPONDING TO THE ROOTS OF THE CHARACTERISTIC EQUATION ANALYSIS OF THE ROOTS OF THE CHARACTERISTIC EQUATION |
| Record Nr. | UNINA-9910789585803321 |
Babister A. W.
|
||
| Oxford, England : , : Pergamon Press, , 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft dynamic stability and response / / A. W. Babister
| Aircraft dynamic stability and response / / A. W. Babister |
| Autore | Babister A. W. |
| Edizione | [First edition.] |
| Pubbl/distr/stampa | Oxford, England : , : Pergamon Press, , 1986 |
| Descrizione fisica | 1 online resource (247 p.) |
| Disciplina | 629.13236 |
| Collana | Pergamon International Library of Science, Technology, Engineering and Social Studies |
| Soggetto topico |
Stability of airplanes
Airplanes - Handling characteristics |
| ISBN | 1-4831-4035-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Dynamic Stability and Response; Copyright Page; Table of Contents; Preface; List Of Symbols; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; UNITS; Part I: FLIGHT DYNAMICS; Chapter 1.INTRODUCTION; THE GENERAL MEANING OF STABILITY; LONGITUDINAL STATIC STABILITY; STATIC MARGIN; STABILITY AND TRIM; MANOEUVRABILITY AND MANOEUVRE MARGIN; REFERENCES; PROBLEMS; Chapter 2. THE EQUATIONS OF MOTION; INTRODUCTION; THE GENERAL DYNAMICAL EQUATIONS FOR A RIGID AIRCRAFT REFERRED TO MOVING AXES
DEFINITION OF THE ANGLE OF PITCH θ, THE ANGLE OF BANK Φ AND ANGLE OF YAW ψRELATIONS FOR RATES OF ROLL, PITCH AND YAW; DETERMINATION OF THE GRAVITATIONAL FORCES; ANGLES OF YAW AND SIDESLIP; DETERMINATION OF THE AERODYNAMIC FORCES; SEPARABILITY OF LONGITUDINAL AND LATERAL MOTION; AXIS SYSTEMS USED IN STABILITY ANALYSIS; NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LONGITUDINAL); NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LATERAL); NON-DIMENSIONAL DISTURBANCES; NON-DIMENSIONAL MASS AND INERTIA; NON-DIMENSIONAL FORM OF THE EQUATIONS OF MOTION; THE MOTION OF THE CENTRE OF GRAVITY OF THE AIRCRAFT REFERENCESPROBLEMS; Chapter 3. AERODYNAMIC DERIVATIVES (LONGITUDINAL); INTRODUCTION; FORCE VELOCITY DERIVATIVES Xu, Xw, Zu, Zw; INCIDENCE CHANGE ASSOCIATED WITH CHANGE IN VELOCITY COMPONENTS; PITCHING MOMENT DERIVATIVES Mu, Mw; DERIVATIVES DUE TO RATE OF PITCH Xq, Zq, Mq; DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY X'w, Z'w, M'w; CONTROL DERIVATIVES; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; AMERICAN NON-DIMENSIONAL FORCE-VELOCITY DERIVATIVES cxu, cxα, czu, czα,; AMERICAN NON-DIMENSIONAL PITCHING MOMENT DERIVATIVES Cmu, Cma AMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF PITCH cxq, czq, cmqAMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY CxDα, CzDα, CmDα; AMERICAN NON-DIMENSIONAL CONTROL DERIVATIVES Cxδe, CZδe, Cmδe DUE TO ELEVATOR; REFERENCES; PROBLEMS; Chapter 4. AERODYNAMIC DERIVATIVES (LATERAL); INTRODUCTION; ESTIMATION OF LATERAL STABILITY DERIVATIVES; DERIVATIVES DUE TO SIDESLIP; DERIVATIVES DUE TO RATE OF ROLL; DERIVATIVES DUE TO RATE OF YAW; CONTROL DERIVATIVES; DERIVATIVES DUE TO AILERONS; DERIVATIVES DUE TO RUDDER NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICANON-DIMENSIONAL FORMS OF THE CONTROL DERIVATIVES USED IN AMERICA; REFERENCES; PROBLEMS; Part II: LONGITUDINAL DYNAMIC STABILITY AND RESPONSE; Chapter 5. BASIC LONGITUDINAL MOTIONS; INTRODUCTION; THE SHORT PERIOD OSCILLATION; THE PHUGOID (LONG PERIOD) OSCILLATION; PROBLEMS; Chapter 6. LONGITUDINAL DYNAMIC STABILITY; INTRODUCTION; STICK FIXED DYNAMIC STABILITY; THE GENERAL SOLUTION OF THE EQUATIONS OF MOTION; TYPES OF MOTION CORRESPONDING TO THE ROOTS OF THE CHARACTERISTIC EQUATION ANALYSIS OF THE ROOTS OF THE CHARACTERISTIC EQUATION |
| Record Nr. | UNINA-9910819946403321 |
|
Babister A. W.
|
||
| Oxford, England : , : Pergamon Press, , 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||