01189nas a2200277 i 450099100259465970753620240521105212.0011205c19899999it qr p 0 0eng d0394-9370b11681287-39ule_instPERLE003470ExLCDU 577Ethology, ecology and evolutionEthology, ecology and evolution /Università degli Studi, Firenze. Dipartimento di Biologia Animale e Genetica. - 1989-Firenze,1989-Codice CNR: P 00064560LE003 1989-2013;Università degli Studi <Firenze> :Dipartimento di Biologia Animale e Geneticaauthorhttp://id.loc.gov/vocabulary/relators/aut316819Monitore zoologico italianohttp://www.tandfonline.com/loi/teee20Abstract available from 1997- on Site of Taylor&Francis Group.b1168128714-11-1908-07-02991002594659707536LE003 (Fondo SBM)1le003-E0.00-n-180000.i1190941908-07-02Ethology, ecology and evolution1745863UNISALENTOle00301-01-01sa-engit0105547nam 22007333u 450 991100660660332120230802010937.00-486-14165-91-62198-609-8(CKB)2550000001187262(EBL)1900927(SSID)ssj0000956080(PQKBManifestationID)12397765(PQKBTitleCode)TC0000956080(PQKBWorkID)10957082(PQKB)11422115(MiAaPQ)EBC1900927(Au-PeEL)EBL1900927(CaONFJC)MIL566633(OCoLC)868272500(EXLCZ)99255000000118726220141229d2012|||| u|| |engur|n|---|||||txtccrDynamics of Atmospheric Flight1st ed.Newburyport Dover Publications20121 online resource (833 p.)Dover Books on Aeronautical EngineeringDescription based upon print version of record.0-486-44522-4 1-306-35382-3 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 SYSTEMSCHAPTER 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 SYSTEM5.5 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 FORCES6.2 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 STIFFNESS7.4 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 flight9.1 LONGITUDINAL MODESGeared toward upper-level undergrads, graduate students, and practicing engineers, this comprehensive treatment of the dynamics of atmospheric flight focuses especially on the stability and control of airplanes. An extensive set of numerical examples covers STOL airplanes, subsonic jet transports, hypersonic flight, stability augmentation, and wind and density gradients.The equations of motion receive a very full treatment, including the effects of the curvature and rotation of the Earth and distortional motion. Complete chapters are given to human pilots and handling qualities and to flight iDover Books on Aeronautical EngineeringAerodynamicsStability of airplanesFlightMechanical EngineeringHILCCEngineering & Applied SciencesHILCCAeronautics Engineering & AstronauticsHILCCAerodynamics.Stability of airplanes.Flight.Mechanical EngineeringEngineering & Applied SciencesAeronautics Engineering & Astronautics629.132/3Etkin Bernard3905AU-PeELAU-PeELAU-PeELBOOK9911006606603321Dynamics of atmospheric flight1422644UNINA