LEADER 05547nam 22007333u 450 001 9911006606603321 005 20230802010937.0 010 $a0-486-14165-9 010 $a1-62198-609-8 035 $a(CKB)2550000001187262 035 $a(EBL)1900927 035 $a(SSID)ssj0000956080 035 $a(PQKBManifestationID)12397765 035 $a(PQKBTitleCode)TC0000956080 035 $a(PQKBWorkID)10957082 035 $a(PQKB)11422115 035 $a(MiAaPQ)EBC1900927 035 $a(Au-PeEL)EBL1900927 035 $a(CaONFJC)MIL566633 035 $a(OCoLC)868272500 035 $a(EXLCZ)992550000001187262 100 $a20141229d2012|||| u|| | 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aDynamics of Atmospheric Flight 205 $a1st ed. 210 $aNewburyport $cDover Publications$d2012 215 $a1 online resource (833 p.) 225 1 $aDover Books on Aeronautical Engineering 300 $aDescription based upon print version of record. 311 08$a0-486-44522-4 311 08$a1-306-35382-3 327 $aTitle 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 327 $aCHAPTER 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 327 $a5.5 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 327 $a6.2 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 327 $a7.4 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 ? DERIVATIVES; 8.6 THE p DERIVATIVES; 8.7 THE r DERIVATIVES; 8.8 SUMMARY OF THE FORMULAE; CHAPTER 9 - Stability of steady flight 327 $a9.1 LONGITUDINAL MODES 330 $aGeared toward upper-level undergrads, graduate students, and practicing engineers, this comprehensive treatment of the dynamics of atmospheric flight focuses especially on the stability and control of airplanes. An extensive set of numerical examples covers STOL airplanes, subsonic jet transports, hypersonic flight, stability augmentation, and wind and density gradients.The equations of motion receive a very full treatment, including the effects of the curvature and rotation of the Earth and distortional motion. Complete chapters are given to human pilots and handling qualities and to flight i 410 0$aDover Books on Aeronautical Engineering 606 $aAerodynamics 606 $aStability of airplanes 606 $aFlight 606 $aMechanical Engineering$2HILCC 606 $aEngineering & Applied Sciences$2HILCC 606 $aAeronautics Engineering & Astronautics$2HILCC 615 0$aAerodynamics. 615 0$aStability of airplanes. 615 0$aFlight. 615 7$aMechanical Engineering 615 7$aEngineering & Applied Sciences 615 7$aAeronautics Engineering & Astronautics 676 $a629.132/3 700 $aEtkin$b Bernard$03905 801 0$bAU-PeEL 801 1$bAU-PeEL 801 2$bAU-PeEL 906 $aBOOK 912 $a9911006606603321 996 $aDynamics of atmospheric flight$91422644 997 $aUNINA