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Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes / / by John M. Riebe and Rodger L. Naeseth
| Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes / / by John M. Riebe and Rodger L. Naeseth |
| Autore | Riebe John M. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica | 1 online resource (48 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Seaplanes - Aerodynamics
Seaplanes - Hulls Planing hulls Stability of airplanes |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713753703321 |
Riebe John M.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section / / by Alvin H. Sacks
| Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section / / by Alvin H. Sacks |
| Autore | Sacks Alvin H. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 |
| Descrizione fisica | 1 online resource (74 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamics
Airplanes Mathematical analysis Stability of airplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713886503321 |
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Sacks Alvin H.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954 | ||
| 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 | ||
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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-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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Aircraft Weight and Balance Handbook : FAA-H-8083-1A
| Aircraft Weight and Balance Handbook : FAA-H-8083-1A |
| Autore | Administration Federal Aviation |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | New York, : Skyhorse Publishing, 2011 |
| Descrizione fisica | 1 online resource (208 p.) |
| Disciplina |
629.134/52
629.13452 |
| Soggetto topico |
Airplanes -- Weight -- Handbooks, manuals, etc
Airplanes Stability of airplanes -- Handbooks, manuals, etc Stability of airplanes Stability of airplanes - Weight Mechanical Engineering Engineering & Applied Sciences Aeronautics Engineering & Astronautics |
| Soggetto genere / forma | Handbooks and manuals. |
| ISBN | 1-62636-681-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page; Copyright Page; Preface; Introduction; Table of Contents; Chapter 1 - Weight and Balance Control; Weight Control; Effects of Weight; Weight Changes; Stability and Balance Control; Weight Control for Aircraft other than Fixed and Rotorwing; Chapter 2 - Weight and Balance Theory and Documentation; Weight and Balance Theory; Aircraft Arms, Weight, and Moments; The Law of the Lever; Determining the CG; Shifting the CG; Basic Weight and Balance Equation; Shifting the Airplane CG; Weight and Balance Documentation; Manufacturer-Furnished Information
Chapter 3 - Weighing the Aircraft and Determining the Empty Weight-Center of GravityRequirements; Equipment for Weighing; Preparation for Weighing; Safety Considerations; Determining the Center of Gravity; Empty-Weight Center of Gravity Formulas; Chapter 4 - Small Fixed Wing Aircraft Operational Weight and Balance Computations; Determining the Loaded Weight and CG; Multiengine Airplane Weight and Balance Computations; Chapter 5 - Center of Gravity Change after Repair or Alterations; Equipment List; Weight and Balance Revision Record; Weight Changes Caused by a Repair or Alteration Empty-Weight CG RangeAdverse-Loaded CG Checks; Chapter 6 - Weight and Balance Control - Helicopter; Determining the Loaded CG of a Helicopter; Chapter 7 - Large Aircraft Weight and Balance; Weighing Procedures; Determining the Empty Weight and EWCG; Determining the Correct Stabilizer Trim Setting; Determining CG Changes Caused by Modifying the Cargo; Effects of Onloading Cargo; Determining Cargo Pallet Loads with Regard to Floor Loading Limits; Determining the Maximum Amount of Payload That Can Be Carried; Determining the Landing Weight; Determining the Minutes of Fuel Dump Time Weight and Balance of Commuter Category AirplanesChapter 8 - Use of Computer for Weight and Balance Computations; Using an Electronic Calculator to Solve Weight and Balance Problems; Using an E6-B Flight Computer to Solve Weight and Balance Problems; Using a Dedicated Electronic Flight Computer to Solve Weight and Balance Problems; Determining CG in Inches From the Datum; Determining CG, Given Weights and Arms; Appendix - Supplemental Study Materials for Aircraft Weight and Balance; Glossary; Index |
| Altri titoli varianti | Aircraft Weight and Balance Handbook |
| Record Nr. | UNINA-9910698557103321 |
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Administration Federal Aviation
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| New York, : Skyhorse Publishing, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analysis of wind-tunnel data on directional stability and control / / by H.R. Pass
| Analysis of wind-tunnel data on directional stability and control / / by H.R. Pass |
| Autore | Pass H. R. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics ; , 1940 |
| Descrizione fisica | 1 online resource (33 pages, 19 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Stability of airplanes
Airplanes - Control Airplanes - Tail surfaces Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717113903321 |
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Pass H. R.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics ; , 1940 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The behavior of conventional airplanes in situations thought to lead to most crashes / / by Fred E. Weick
| The behavior of conventional airplanes in situations thought to lead to most crashes / / by Fred E. Weick |
| Autore | Weick Fred E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931 |
| Descrizione fisica | 1 online resource (13 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aircraft accidents
Stalling (Aerodynamics) Airplanes - Landing Airplanes - Takeoff Stability of airplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715142503321 |
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Weick Fred E.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report / / prepared by W.H. Hui
| Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report / / prepared by W.H. Hui |
| Autore | Hui W. H. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : [National Aeronautics and Space Administration], , 1985 |
| Descrizione fisica | 1 online resource (approximately 48 pages) |
| Collana | [NASA contractor report] |
| Soggetto topico |
Aerofoils
Equations of motion Unsteady flow (Aerodynamics) Stability of airplanes Aerodynamic stability Airfoils Branching (mathematics) Hysteresis Oscillations Unsteady aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack |
| Record Nr. | UNINA-9910715477503321 |
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Hui W. H.
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| [Washington, D.C.] : , : [National Aeronautics and Space Administration], , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamics of Atmospheric Flight
| Dynamics of Atmospheric Flight |
| Autore | Etkin Bernard |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Newburyport, : Dover Publications, 2012 |
| Descrizione fisica | 1 online resource (833 p.) |
| Disciplina | 629.132/3 |
| Collana | Dover Books on Aeronautical Engineering |
| Soggetto topico |
Aerodynamics
Stability of airplanes Flight Mechanical Engineering Engineering & Applied Sciences Aeronautics Engineering & Astronautics |
| ISBN |
0-486-14165-9
1-62198-609-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page; Copyright Page; Preface; Table of Contents; CHAPTER I - Introduction; TYPES OF PROBLEMS; THE TOOLS OF FLIGHT DYNAMICISTS; CHAPTER 2 - Analytical tools; 2.1 INTRODUCTION; 2.2 VECTOR/MATRIX ALGEBRA; 2.3 LAPLACE AND FOURIER TRANSFORMS; 2.4 APPLICATION TO DIFFERENTIAL EQUATIONS; 2.5 METHODS FOR THE INVERSE TRANSFORMATION; 2.6 RANDOM PROCESS THEORY; 2.7 MACHINE COMPUTATION; CHAPTER 3 - Systems Theory; 3.1 CONCEPTS AND TERMINOLOGY; 3.2 TRANSFER FUNCTIONS; 3.3 AUTONOMOUS LINEAR/INVARIANT SYSTEMS; 3.4 RESPONSE OF LINEAR/INVARIANT SYSTEMS; 3.5 TIME-VARYING AND NONLINEAR SYSTEMS
CHAPTER 4 - Reference frames and transformations4.1 NOTATION; 4.2 DEFINITIONS OF REFERENCE FRAMES USED IN VEHICLE DYNAMICS; 4.3 DEFINITION OF THE ANGLES; 4.4 TRANSFORMATION OF A VECTOR; 4.5 THE L MATRIX IN TERMS OF ROTATION ANGLES; 4.6 TRANSFORMATION OF THE DERIVATIVE OF A VECTOR; 4.7 TRANSFORMATION OF A MATRIX; CHAPTER 5 - General equations of unsteady motion; 5.1 VELOCITY AND ACCELERATION IN AN ARBITRARILY MOVING FRAME; 5.2 ANGULAR VELOCITIES OF THE SEVERAL REFERENCE FRAMES; 5.3 POSITION, VELOCITY, AND ACCELERATION OF THE VEHICLE MASS CENTER; 5.4 EQUATIONS OF MOTION OF AN ARBITRARY SYSTEM 5.5 FORCE EQUATIONS IN WIND AXES5.6 FORCE AND MOMENT EQUATIONS IN BODY AXES (EULER'S EQUATIONS); 5.7 DISCUSSION OF THE SYSTEM OF EQUATIONS; 5.8 THE FLAT-EARTH APPROXIMATION; 5.9 STEADY STATES; 5.10 THE SMALL-DISTURBANCE THEORY; 5.11 EXACT LINEAR AERODYNAMICS AND THE TRANSFORMED EQUATIONS; 5.13 NONDIMENSIONAL EQUATIONS; 5.14 TRANSFORMS OF THE NONDIMENSIONAL EQUATIONS; 5.15 TRANSFORMATION OF AERODYNAMIC DERIVATIVES FROM ONE BODY-FIXED REFERENCE FRAME TO ANOTHER; CHAPTER 6 - Longitudinal aerodynamic characteristics-part 1; 6.1 THE BASIC LONGITUDINAL FORCES 6.2 PITCH STIFFNESS AND POSSIBLE CONFIGURATIONS FOR FLIGHT6.3 PITCH STIFFNESS OF A GENERAL CONFIGURATION; 6.4 LONGITUDINAL CONTROL; 6.5 CONTROL HINGE MOMENT; 6.6 INFLUENCE OF A FREE ELEVATOR ON LIFT AND MOMENT; 6.7 THE USE OF TABS; 6.8 CONTROL FORCE TO TRIM; 6.9 CONTROL FORCE GRADIENT; 6.10 MANEUVERABILlTY-ELEVATOR ANGLE AND CONTROL FORCE PER g; CHAPTER 7 - Longitudinal aerodynamic characteristics-part 2; 7.1 BOB WEIGHTS AND SPRINGS; 7.2 INFLUENCE OF HIGH-LIFT DEVICES ON TRIM AND PITCH STIFFNESS; 7.3 INFLUENCE OF THE PROPULSIVE SYSTEM ON TRIM AND PITCH STIFFNESS 7.4 EFFECT OF STRUCTURAL FLEXIBILITY7.5 GROUND EFFECT; 7.6 C.G. LIMITS; 7.7 LONGITUDINAL AERODYNAMIC DERIVATIVES; 7.8 THE V DERIVATIVES; 7.9 THE q DERIVATIVES; 7.10 THE DERIVATIVES; 7.11 AERODYNAMIC TRANSFER FUNCTIONS; 7.12 THE z DERIVATIVES; 7.13 AEROELASTIC DERIVATIVES; 7.14 SUMMARY OF THE FORMULAE; CHAPTER 8 - Lateral aerodynamic characteristics; 8.1 YAW STIFFNESS (WEATHERCOCK STABILITY); 8.2 YAW CONTROL; 8.3 ROLL STIFFNESS; 8.4 ROLLING CONTROL; 8.5 THE β DERIVATIVES; 8.6 THE p DERIVATIVES; 8.7 THE r DERIVATIVES; 8.8 SUMMARY OF THE FORMULAE; CHAPTER 9 - Stability of steady flight 9.1 LONGITUDINAL MODES |
| Record Nr. | UNINA-9911006606603321 |
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Etkin Bernard
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| Newburyport, : Dover Publications, 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamics of flight : stability and control / Bernard Etkin, Lloyd Duff Reid
| Dynamics of flight : stability and control / Bernard Etkin, Lloyd Duff Reid |
| Autore | Etkin, Bernard |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | New York : Wiley, c1996 |
| Descrizione fisica | xi, 382 p. : ill. ; 26 cm |
| Disciplina | 629.1323 |
| Altri autori (Persone) | Reid, Lloyd Duffauthor |
| Soggetto topico |
Aerodynamics
Stability of airplanes |
| ISBN | 9780471034186 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991000250929707536 |
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Etkin, Bernard
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| New York : Wiley, c1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
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