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Aerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and low supersonic speeds / / by Grady L. Mitcham, Joseph E. Stevens, and Harry P. Norris
| Aerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and low supersonic speeds / / by Grady L. Mitcham, Joseph E. Stevens, and Harry P. Norris |
| Autore | Mitcham Grady L. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1956 |
| Descrizione fisica | 1 online resource (57 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Testing
Tailless airplanes Airplanes - Handling characteristics Aerodynamics, Supersonic Aerodynamics, Transonic |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713876003321 |
Mitcham Grady L.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1956 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Babister A. W.
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| 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 |
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Babister A. W.
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| Oxford, England : , : Pergamon Press, , 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Determination of climbing ability / / by H. Blasius
| Determination of climbing ability / / by H. Blasius |
| Autore | Blasius H. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 |
| Descrizione fisica | 1 online resource (16 pages, 2 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Altitude, Influence of
Airplanes - Handling characteristics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713431503321 |
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Blasius H.
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effects of an autopilot on airplane responses to turbulence with emphasis on tail loads / / by Boyd Perry III
| The effects of an autopilot on airplane responses to turbulence with emphasis on tail loads / / by Boyd Perry III |
| Autore | Perry Boyd |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1973 |
| Descrizione fisica | 1 online resource (i, 51 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerodynamic loads
Atmospheric turbulence Automatic pilot (Airplanes) Airplanes - Handling characteristics Airplanes - Tail surfaces Aerodynamic load |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716544203321 |
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Perry Boyd
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1973 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight characteristics / / by Captain Student
| Flight characteristics / / by Captain Student |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 |
| Descrizione fisica | 1 online resource (8 pages) |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Flight
Airplanes - Handling characteristics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713439403321 |
| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane / / H. Paul Stough III, Daniel J. DiCarlo, and James M. Patton, Jr
| Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane / / H. Paul Stough III, Daniel J. DiCarlo, and James M. Patton, Jr |
| Autore | Stough H. Paul |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1985 |
| Descrizione fisica | 1 online resource (vi, 92 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Aerodynamic stalling
Aerodynamic characteristics Aircraft spin Spin dynamics Flight tests Stalling (Aerodynamics) Spin (Aerodynamics) Airplanes - Handling characteristics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709603003321 |
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Stough H. Paul
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight measurements of buffet characteristics of the F-104 airplane for selected wing-flap deflections / / by Edward L. Friend and Walter J. Sefic
| Flight measurements of buffet characteristics of the F-104 airplane for selected wing-flap deflections / / by Edward L. Friend and Walter J. Sefic |
| Autore | Friend Edward L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , August 1972 |
| Descrizione fisica | 1 online resource (47 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Buffeting
Aerodynamics Buffeting (Aerodynamics) Flaps (Airplanes) Airplanes - Handling characteristics Starfighter (Fighter plane) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716560003321 |
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Friend Edward L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , August 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight tests under IFR with an STOL transport aircraft / / by Robert C. Innis, Curt A. Holzhauser, and Richard P. Gallant
| Flight tests under IFR with an STOL transport aircraft / / by Robert C. Innis, Curt A. Holzhauser, and Richard P. Gallant |
| Autore | Innis Robert C. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 |
| Descrizione fisica | 1 online resource (61 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Flight tests
Transport aircraft Airplanes - Flight testing Airplanes - Handling characteristics Instrument flying Short take-off and landing aircraft |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Flight tests under instrument flight rules with an STOL transport aircraft |
| Record Nr. | UNINA-9910716090603321 |
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Innis Robert C.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Graphic method for calculating the speed and climbing ability of airplanes / / by Adolf Rohrbach and Edwin Lupberger
| Graphic method for calculating the speed and climbing ability of airplanes / / by Adolf Rohrbach and Edwin Lupberger |
| Autore | Rohrbach Adolf |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 |
| Descrizione fisica | 1 online resource (9 pages, 1 unnumbered page) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Handling characteristics
Graphic methods |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713432203321 |
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Rohrbach Adolf
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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