LEADER 05115nam 2200553 450 001 9910789585803321 005 20230120013355.0 010 $a1-4831-4035-0 035 $a(CKB)3710000000026518 035 $a(EBL)1828985 035 $a(MiAaPQ)EBC1828985 035 $a(EXLCZ)993710000000026518 100 $a20141118e19861980 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $2rdacontent 182 $2rdamedia 183 $2rdacarrier 200 10$aAircraft dynamic stability and response /$fA. W. Babister 205 $aFirst edition. 210 1$aOxford, England :$cPergamon Press,$d1986. 210 4$dİ1980 215 $a1 online resource (247 p.) 225 1 $aPergamon International Library of Science, Technology, Engineering and Social Studies 300 $aDescription based upon print version of record. 311 $a1-322-27384-7 311 $a0-08-024768-7 320 $aIncludes bibliographical references at the end of each chapters and index. 327 $aFront 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 327 $aDEFINITION OF THE ANGLE OF PITCH ?, THE ANGLE OF BANK ? AND ANGLE OF YAW ?RELATIONS 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 327 $aREFERENCESPROBLEMS; 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, cx?, czu, cz?,; AMERICAN NON-DIMENSIONAL PITCHING MOMENT DERIVATIVES Cmu, Cma 327 $aAMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF PITCH cxq, czq, cmqAMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY CxD?, CzD?, CmD?; AMERICAN NON-DIMENSIONAL CONTROL DERIVATIVES Cx?e, CZ?e, Cm?e 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 327 $aNON-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 327 $aANALYSIS OF THE ROOTS OF THE CHARACTERISTIC EQUATION 330 $aAircraft Dynamic Stability and Response deals with the fundamentals of dynamic stability in aircraft. Topics covered include flight dynamics, equations of motion, and lateral and longitudinal aerodynamic derivatives. Basic lateral and longitudinal motions are also considered. A non-dimensional system of notation is used, and problems are included at the end of chapters. This book is comprised of 13 chapters and begins with an introduction to aircraft static stability and maneuverability, with emphasis on the theoretical basis of flight dynamics and the technical terms used. The physical backgr 410 0$aPergamon international library of science, technology, engineering, and social studies. 606 $aStability of airplanes 606 $aAirplanes$xHandling characteristics 615 0$aStability of airplanes. 615 0$aAirplanes$xHandling characteristics. 676 $a629.13236 700 $aBabister$b A. W.$012687 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910789585803321 996 $aAircraft dynamic stability and response$93710440 997 $aUNINA