{"product_id":"flight-theory-and-aerodynamics-isbn-9781394282296","title":"Flight Theory and Aerodynamics","description":"\u003cp\u003e\u003cb\u003eComprehensive introduction to aerodynamics applied to different types of modern aircraft, now updated with the latest FAA guidance\u003c\/b\u003e \u003c\/p\u003e\u003cp\u003e\u003ci\u003eFlight Theory and Aerodynamics\u003c\/i\u003e provides an introduction to aerodynamics using practical application to modern aircraft with step-by-step calculations. This fifth edition streamlines content, notably the chapters on aircraft stability, and incorporates updated FAA guidance and figures from the 2023 \u003ci\u003ePilot’s Handbook of Aeronautical Knowledge\u003c\/i\u003e as well as other FAA handbooks. \u003c\/p\u003e\u003cp\u003eA balanced application of introductory physics and meteorology in the first five chapters evolves into an introduction to propeller and jet aircraft propulsion and eventually moves into a broad discussion on the application of physics to aircraft takeoff and landing performance. After the introductory material has been presented, principles from earlier in the textbook and prior coursework are correlated and applied to slow flight, aircraft stability, and high-speed flight. A new chapter on Unmanned Aerial Vehicle (UAV) flight theory is included. \u003c\/p\u003e\u003cp\u003eThe text features extensive instructor resources including detailed PowerPoint slides for each chapter, step-by-step guidance for end of chapter calculations, sample test bank questions for each chapter, and application sections within each chapter that allow the instructor to challenge the student with additional real-world scenarios based on chapter content. \u003c\/p\u003e\u003cp\u003e\u003ci\u003eFlight Theory and Aerodynamics\u003c\/i\u003e includes information on: \u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eElements of the flight environment, covering forces, mass, scalar and vector quantities, linear and rotational motion, friction, and power\u003c\/li\u003e\n\u003cli\u003eAtmosphere, altitude, and airspeed measurement, covering properties of the atmosphere, Bernoulli’s equation, and pitot-static system advantages and disadvantages\u003c\/li\u003e\n\u003cli\u003eJet aircraft performance, covering principles of propulsion, fuel flow, specific fuel consumption, and thrust-required curves\u003c\/li\u003e\n\u003cli\u003eAircraft stability and control, covering oscillatory motion, weight and balance, and airplane reference axes\u003c\/li\u003e\n\u003cli\u003eRotary-wing flight theory, airfoil selection, and helicopter control\u003c\/li\u003e\n\u003cli\u003eUAV flight theory, including UAV design considerations, the aerodynamics of UAV fuselage design, UAV powerplant design, and the future of UAV design and aerodynamics\u003c\/li\u003e\n\u003cli\u003eEnd of chapter questions focused on scenario-based learning as applied to the performance analysis of a Diamond DA50 and corresponding chapter material.\u003c\/li\u003e\n\u003c\/ul\u003e \u003cp\u003eIn addition to degree-oriented college programs, this latest edition of \u003ci\u003eFlight Theory and Aerodynamics\u003c\/i\u003e is also an essential resource for pilot training programs ranging from student pilots to flight instructors as well as practicing professionals flying a wide range of aircraft. \u003c\/p\u003e\u003cp\u003e1 Introduction to the Flight Environment. 15\u003c\/p\u003e \u003cp\u003eIntroduction. 16\u003c\/p\u003e \u003cp\u003eHistory of Aerodynamics. 16\u003c\/p\u003e \u003cp\u003eBasic Quantities. 21\u003c\/p\u003e \u003cp\u003eForces. 22\u003c\/p\u003e \u003cp\u003eMass. 24\u003c\/p\u003e \u003cp\u003eScalar and Vector Quantities. 24\u003c\/p\u003e \u003cp\u003eScalar Addition. 24\u003c\/p\u003e \u003cp\u003eVector Addition. 25\u003c\/p\u003e \u003cp\u003eVector Resolution. 26\u003c\/p\u003e \u003cp\u003eMoments. 27\u003c\/p\u003e \u003cp\u003eEquilibrium Conditions. 28\u003c\/p\u003e \u003cp\u003eNewton’s Laws of Motion. 29\u003c\/p\u003e \u003cp\u003eNewton’s First Law.. 29\u003c\/p\u003e \u003cp\u003eNewton’s Second Law.. 29\u003c\/p\u003e \u003cp\u003eNewton’s Third Law.. 30\u003c\/p\u003e \u003cp\u003eEnergy and Work. 30\u003c\/p\u003e \u003cp\u003ePower. 31\u003c\/p\u003e \u003cp\u003eFriction. 32\u003c\/p\u003e \u003cp\u003eIntroduction to Linear Motion. 33\u003c\/p\u003e \u003cp\u003eintroduction to Rotational Motion. 35\u003c\/p\u003e \u003cp\u003eCHAPTER 1 Symbols. 36\u003c\/p\u003e \u003cp\u003eCHAPTER 1 EQUATIONS. 37\u003c\/p\u003e \u003cp\u003eCHAPTER 1 KEY TERMS. 37\u003c\/p\u003e \u003cp\u003eCHAPTER 1 PROBLEMS. 39\u003c\/p\u003e \u003cp\u003eCHAPTER 1 BIBLIOGRAPHY. 42\u003c\/p\u003e \u003cp\u003e2 Atmosphere, Altitude, and Airspeed Measurement. 44\u003c\/p\u003e \u003cp\u003ePROPERTIES OF THE ATMOSPHERE. 44\u003c\/p\u003e \u003cp\u003eStatic Pressure. 45\u003c\/p\u003e \u003cp\u003eTemperature. 46\u003c\/p\u003e \u003cp\u003eDensity. 48\u003c\/p\u003e \u003cp\u003eViscosity. 50\u003c\/p\u003e \u003cp\u003eICAO Standard Atmosphere. 50\u003c\/p\u003e \u003cp\u003eAltitude Measurement. 51\u003c\/p\u003e \u003cp\u003eIndicated Altitude. 51\u003c\/p\u003e \u003cp\u003eCalibrated Altitude. 52\u003c\/p\u003e \u003cp\u003eTrue Altitude. 52\u003c\/p\u003e \u003cp\u003eAbsolute Altitude. 52\u003c\/p\u003e \u003cp\u003ePressure Altitude. 53\u003c\/p\u003e \u003cp\u003eDensity Altitude. 54\u003c\/p\u003e \u003cp\u003eContinuity Equation. 56\u003c\/p\u003e \u003cp\u003eBernoulli's Equation. 57\u003c\/p\u003e \u003cp\u003eAirspeed Measurement. 60\u003c\/p\u003e \u003cp\u003eIndicated Airspeed. 63\u003c\/p\u003e \u003cp\u003eCalibrated Airspeed. 63\u003c\/p\u003e \u003cp\u003eEquivalent Airspeed. 64\u003c\/p\u003e \u003cp\u003eTrue Airspeed. 64\u003c\/p\u003e \u003cp\u003eMach. 66\u003c\/p\u003e \u003cp\u003eGroundspeed. 67\u003c\/p\u003e \u003cp\u003eCHAPTER 2 Symbols. 67\u003c\/p\u003e \u003cp\u003eCHAPTER 2 EQUATIONS. 68\u003c\/p\u003e \u003cp\u003eCHAPTER 2 KEY TERMS. 69\u003c\/p\u003e \u003cp\u003eCHAPTER 2 PROBLEMS. 70\u003c\/p\u003e \u003cp\u003eCHAPTER 2 BIBLIOGRAPHY. 74\u003c\/p\u003e \u003cp\u003e3 Structures, Airfoils, and Aerodynamic Forces. 75\u003c\/p\u003e \u003cp\u003eAIRCRAFT STRUCTURES. 75\u003c\/p\u003e \u003cp\u003ePrimary Flight Controls. 76\u003c\/p\u003e \u003cp\u003eSecondary Flight Controls. 83\u003c\/p\u003e \u003cp\u003eAIRFOILS. 89\u003c\/p\u003e \u003cp\u003eAirfoil Terminology. 90\u003c\/p\u003e \u003cp\u003eDefinitions. 90\u003c\/p\u003e \u003cp\u003eGeometry Variables of Airfoils. 91\u003c\/p\u003e \u003cp\u003eClassification of Airfoils. 93\u003c\/p\u003e \u003cp\u003eDEVELOPMENT OF FORCES ON AIRFOILS. 96\u003c\/p\u003e \u003cp\u003ePressure Disturbances on Airfoils. 96\u003c\/p\u003e \u003cp\u003eVelocity and Static Pressure Changes about an Airfoil 97\u003c\/p\u003e \u003cp\u003eAERODYNAMIC FORCE. 98\u003c\/p\u003e \u003cp\u003ePressure Distribution on a Rotating Cylinder. 98\u003c\/p\u003e \u003cp\u003eAERODYNAMIC PITCHING MOMENTS. 99\u003c\/p\u003e \u003cp\u003eAERODYNAMIC CENTER. 102\u003c\/p\u003e \u003cp\u003eACCIDENT BRIEF: AIR MIDWEST FLIGHT 5481. 103\u003c\/p\u003e \u003cp\u003eCHAPTER 3 SYMBOLS. 104\u003c\/p\u003e \u003cp\u003eCHAPTER 3 KEY TERMS. 104\u003c\/p\u003e \u003cp\u003eCHAPTER 3 PROBLEMS. 105\u003c\/p\u003e \u003cp\u003eCHAPTER 3 BIBLIOGRAPHY. 109\u003c\/p\u003e \u003cp\u003e4 Lift. 110\u003c\/p\u003e \u003cp\u003eIntroduction to Lift. 110\u003c\/p\u003e \u003cp\u003eAngle of Attack. 111\u003c\/p\u003e \u003cp\u003eAngle of Attack Indicator. 112\u003c\/p\u003e \u003cp\u003eAccident Brief: Air France Flight 447. 114\u003c\/p\u003e \u003cp\u003eAngle of Attack and Coefficient of Lift. 115\u003c\/p\u003e \u003cp\u003eBoundary Layer Theory. 116\u003c\/p\u003e \u003cp\u003eCoanda Effect. 119\u003c\/p\u003e \u003cp\u003eReynolds Number. 119\u003c\/p\u003e \u003cp\u003eAdverse Pressure Gradient. 121\u003c\/p\u003e \u003cp\u003eAirflow Separation. 122\u003c\/p\u003e \u003cp\u003eStall 124\u003c\/p\u003e \u003cp\u003eAerodynamic Force Equations. 126\u003c\/p\u003e \u003cp\u003eLift Equation. 126\u003c\/p\u003e \u003cp\u003eCoefficient of Lift and the Lift Equation. 127\u003c\/p\u003e \u003cp\u003eVelocity. 129\u003c\/p\u003e \u003cp\u003eLift Formula Summary. 131\u003c\/p\u003e \u003cp\u003eAirfoil Lift Characteristics. 132\u003c\/p\u003e \u003cp\u003eHigh Coefficient of Lift Devices. 133\u003c\/p\u003e \u003cp\u003eEffect of Ice and Frost. 141\u003c\/p\u003e \u003cp\u003eLift During Flight Maneuvers. 142\u003c\/p\u003e \u003cp\u003eLift During Turns. 143\u003c\/p\u003e \u003cp\u003eLift During Climbs and Descents. 144\u003c\/p\u003e \u003cp\u003eLift and Balloons. 145\u003c\/p\u003e \u003cp\u003eCHAPTER 4 Symbols. 147\u003c\/p\u003e \u003cp\u003eCHAPTER 4 EQUATIONS. 148\u003c\/p\u003e \u003cp\u003eCHAPTER 4 KEY TERMS. 148\u003c\/p\u003e \u003cp\u003eCHAPTER 4 PROBLEMS. 149\u003c\/p\u003e \u003cp\u003eCHAPTER 4 BIBLIOGRAPHY. 153\u003c\/p\u003e \u003cp\u003e5 Drag. 155\u003c\/p\u003e \u003cp\u003eInduced Drag. 155\u003c\/p\u003e \u003cp\u003eAspect Ratio. 158\u003c\/p\u003e \u003cp\u003eWingtip Vortices. 160\u003c\/p\u003e \u003cp\u003eInfinite Wing. 161\u003c\/p\u003e \u003cp\u003eFinite Wing. 162\u003c\/p\u003e \u003cp\u003eInduced Drag Summary. 164\u003c\/p\u003e \u003cp\u003eGround Effect. 165\u003c\/p\u003e \u003cp\u003eAirflow Alteration Around the Wing. 166\u003c\/p\u003e \u003cp\u003ePitching Moments. 167\u003c\/p\u003e \u003cp\u003ePitot–Static Influence. 168\u003c\/p\u003e \u003cp\u003eGround Effect Summary. 168\u003c\/p\u003e \u003cp\u003eParasite Drag. 170\u003c\/p\u003e \u003cp\u003eSkin Friction Drag. 170\u003c\/p\u003e \u003cp\u003eLaminar Flow Airfoils. 171\u003c\/p\u003e \u003cp\u003eForm Drag. 174\u003c\/p\u003e \u003cp\u003eInterference Drag. 175\u003c\/p\u003e \u003cp\u003eLeakage Drag. 176\u003c\/p\u003e \u003cp\u003eParasite Drag Summary. 176\u003c\/p\u003e \u003cp\u003eDrag Equation. 177\u003c\/p\u003e \u003cp\u003eInduced and Parasite Drag Calculations. 178\u003c\/p\u003e \u003cp\u003eTotal Drag. 179\u003c\/p\u003e \u003cp\u003eLift-to-Drag Ratio. 181\u003c\/p\u003e \u003cp\u003e(\u003ci\u003eL\u003c\/i\u003e\/\u003ci\u003eD\u003c\/i\u003e)maxSummary. 185\u003c\/p\u003e \u003cp\u003eDrag Reduction. 186\u003c\/p\u003e \u003cp\u003eWinglet Design. 186\u003c\/p\u003e \u003cp\u003eWinglet Application. 189\u003c\/p\u003e \u003cp\u003eCHAPTER 5 Symbols. 190\u003c\/p\u003e \u003cp\u003eCHAPTER 5 EQUATIONS. 191\u003c\/p\u003e \u003cp\u003eCHAPTER 5 KEY TERMS. 191\u003c\/p\u003e \u003cp\u003eCHAPTER 5 PROBLEMS. 193\u003c\/p\u003e \u003cp\u003eCHAPTER 5 BIBLIOGRAPHY. 197\u003c\/p\u003e \u003cp\u003e6 Jet Aircraft Performance. 199\u003c\/p\u003e \u003cp\u003eThrust-Producing Aircraft. 200\u003c\/p\u003e \u003cp\u003eTurbine Engine Operation. 201\u003c\/p\u003e \u003cp\u003eThrust-Required Curve. 203\u003c\/p\u003e \u003cp\u003ePrinciples of Propulsion. 204\u003c\/p\u003e \u003cp\u003eThrust-Available Turbojet Aircraft. 206\u003c\/p\u003e \u003cp\u003eThrust Variation and rpm.. 206\u003c\/p\u003e \u003cp\u003eSpecific Fuel Consumption. 209\u003c\/p\u003e \u003cp\u003eFuel Flow.. 211\u003c\/p\u003e \u003cp\u003eThrust-Available\/Thrust-Required Curves. 211\u003c\/p\u003e \u003cp\u003eItems of Aircraft Performance. 212\u003c\/p\u003e \u003cp\u003eStraight and Level Flight. 212\u003c\/p\u003e \u003cp\u003eClimb Performance. 213\u003c\/p\u003e \u003cp\u003eAngle of Climb. 214\u003c\/p\u003e \u003cp\u003eRate of Climb. 215\u003c\/p\u003e \u003cp\u003eEndurance. 218\u003c\/p\u003e \u003cp\u003eSpecific Range. 219\u003c\/p\u003e \u003cp\u003eWind Effect on Specific Range. 220\u003c\/p\u003e \u003cp\u003eTotal Range. 220\u003c\/p\u003e \u003cp\u003eVariations in the Thrust-Required Curve. 221\u003c\/p\u003e \u003cp\u003eWeight Changes. 222\u003c\/p\u003e \u003cp\u003eConfiguration Changes. 226\u003c\/p\u003e \u003cp\u003eAltitude Changes. 228\u003c\/p\u003e \u003cp\u003eCruise–Climb Flight. 230\u003c\/p\u003e \u003cp\u003eAfterburners and Vectored Thrust. 231\u003c\/p\u003e \u003cp\u003eJet Performance Summary. 232\u003c\/p\u003e \u003cp\u003eCHAPTER 6 Symbols. 233\u003c\/p\u003e \u003cp\u003eCHAPTER 6 EQUATIONS. 234\u003c\/p\u003e \u003cp\u003eCHAPTER 6 KEY TERMS. 235\u003c\/p\u003e \u003cp\u003eCHAPTER 6 PROBLEMS. 235\u003c\/p\u003e \u003cp\u003eCHAPTER 6 BIBLIOGRAPHY. 239\u003c\/p\u003e \u003cp\u003e7 Propeller Aircraft Performance. 241\u003c\/p\u003e \u003cp\u003ePOWER AVAILABLE. 242\u003c\/p\u003e \u003cp\u003eBasic Propeller Principles. 243\u003c\/p\u003e \u003cp\u003eFixed-Pitch Propeller. 245\u003c\/p\u003e \u003cp\u003eConstant-Speed Propeller. 246\u003c\/p\u003e \u003cp\u003ePRINCIPLES OF PROPULSION.. 248\u003c\/p\u003e \u003cp\u003ePOWER-REQUIRED CURVES. 251\u003c\/p\u003e \u003cp\u003ePower Available Versus Velocity. 253\u003c\/p\u003e \u003cp\u003eVariations with Power and Altitude. 255\u003c\/p\u003e \u003cp\u003eITEMS OF AIRCRAFT PERFORMANCE. 258\u003c\/p\u003e \u003cp\u003eStraight and Level Flight. 258\u003c\/p\u003e \u003cp\u003eClimb Performance. 258\u003c\/p\u003e \u003cp\u003eAngle of Climb. 259\u003c\/p\u003e \u003cp\u003eRate of Climb. 261\u003c\/p\u003e \u003cp\u003eEndurance. 263\u003c\/p\u003e \u003cp\u003eSpecific Range. 265\u003c\/p\u003e \u003cp\u003eWind Effect on Specific Range. 265\u003c\/p\u003e \u003cp\u003eVARIATIONS IN THE POWER-REQUIRED CURVE. 266\u003c\/p\u003e \u003cp\u003eWeight Changes. 266\u003c\/p\u003e \u003cp\u003eConfiguration Change. 270\u003c\/p\u003e \u003cp\u003eAltitude Changes. 272\u003c\/p\u003e \u003cp\u003ePropeller Performance Summary. 276\u003c\/p\u003e \u003cp\u003eCHAPTER 7 SYMBOLS. 277\u003c\/p\u003e \u003cp\u003eCHAPTER 7 EQUATIONS. 278\u003c\/p\u003e \u003cp\u003eCHAPTER 7 KEY TERMS. 278\u003c\/p\u003e \u003cp\u003eCHAPTER 7 PROBLEMS. 279\u003c\/p\u003e \u003cp\u003eChapter 7 Bibliography. 286\u003c\/p\u003e \u003cp\u003e8 Takeoff Performance. 287\u003c\/p\u003e \u003cp\u003eNormal Takeoff. 290\u003c\/p\u003e \u003cp\u003eCrosswind Takeoff. 291\u003c\/p\u003e \u003cp\u003ePerformance Takeoffs. 293\u003c\/p\u003e \u003cp\u003eWater Takeoffs. 295\u003c\/p\u003e \u003cp\u003ePerformance Speeds – Normal Takeoff. 296\u003c\/p\u003e \u003cp\u003eImproper Liftoff. 297\u003c\/p\u003e \u003cp\u003ePremature Takeoff in Ground Effect. 297\u003c\/p\u003e \u003cp\u003eDangers of Over-rotation. 298\u003c\/p\u003e \u003cp\u003eRejected Takeoffs. 298\u003c\/p\u003e \u003cp\u003eRTO V-Speeds and Definitions. 299\u003c\/p\u003e \u003cp\u003eDeclared Distances. 302\u003c\/p\u003e \u003cp\u003eSingle-Engine Airplane. 303\u003c\/p\u003e \u003cp\u003eMulti-Engine Airplane. 304\u003c\/p\u003e \u003cp\u003eRejected Takeoff Aerodynamics. 306\u003c\/p\u003e \u003cp\u003eInitial Climb. 310\u003c\/p\u003e \u003cp\u003eLinear Motion. 313\u003c\/p\u003e \u003cp\u003eFactors Affecting Takeoff Performance. 316\u003c\/p\u003e \u003cp\u003eWeight Change. 316\u003c\/p\u003e \u003cp\u003eAltitude. 318\u003c\/p\u003e \u003cp\u003eWind. 319\u003c\/p\u003e \u003cp\u003eRunway Surface. 322\u003c\/p\u003e \u003cp\u003eRunway Slope. 323\u003c\/p\u003e \u003cp\u003eCHAPTER 8 Symbols. 324\u003c\/p\u003e \u003cp\u003eCHAPTER 8 EQUATIONS. 324\u003c\/p\u003e \u003cp\u003eCHAPTER 8 kEY TERMS. 325\u003c\/p\u003e \u003cp\u003eCHAPTER 8 PROBLEMS. 326\u003c\/p\u003e \u003cp\u003eChapter 8 Bibliography. 331\u003c\/p\u003e \u003cp\u003e9 Landing Performance. 333\u003c\/p\u003e \u003cp\u003ePRELANDING PERFORMANCE. 335\u003c\/p\u003e \u003cp\u003eGliding Flight. 336\u003c\/p\u003e \u003cp\u003eThe Landing Approach. 338\u003c\/p\u003e \u003cp\u003eStabilized Approaches. 339\u003c\/p\u003e \u003cp\u003eApproach Glide Paths. 340\u003c\/p\u003e \u003cp\u003eNORMAL LANDING.. 345\u003c\/p\u003e \u003cp\u003eCrosswind Landing. 345\u003c\/p\u003e \u003cp\u003ePerformance Landings. 347\u003c\/p\u003e \u003cp\u003eIMPROPER LANDING PERFORMANCE. 349\u003c\/p\u003e \u003cp\u003eImproper Round Out. 349\u003c\/p\u003e \u003cp\u003eBouncing and Ballooning. 350\u003c\/p\u003e \u003cp\u003ePorpoising. 351\u003c\/p\u003e \u003cp\u003eRejected Landings (Go-arounds). 352\u003c\/p\u003e \u003cp\u003eHAZARDS OF HYDROPLANING.. 353\u003c\/p\u003e \u003cp\u003eDynamic Hydroplaning. 353\u003c\/p\u003e \u003cp\u003eViscous Hydroplaning. 356\u003c\/p\u003e \u003cp\u003eReverted Rubber Hydroplaning. 356\u003c\/p\u003e \u003cp\u003eLANDING DECELERATION, VELOCITY, AND DISTANCE. 356\u003c\/p\u003e \u003cp\u003eForces on the Aircraft During Landing. 356\u003c\/p\u003e \u003cp\u003eBraking Techniques. 361\u003c\/p\u003e \u003cp\u003eThrust Reversers. 361\u003c\/p\u003e \u003cp\u003eLANDING EQUATIONS. 363\u003c\/p\u003e \u003cp\u003eGeneral Equation. 363\u003c\/p\u003e \u003cp\u003eEffect of Weight Change. 364\u003c\/p\u003e \u003cp\u003eEffect of Altitude. 365\u003c\/p\u003e \u003cp\u003eEffect of Wind. 366\u003c\/p\u003e \u003cp\u003eLANDING ENVIRONMENT. 369\u003c\/p\u003e \u003cp\u003eAccident Brief: Southwest Airlines (SWA) Flight 1248. 369\u003c\/p\u003e \u003cp\u003eRunway Surface. 370\u003c\/p\u003e \u003cp\u003eRunway Slope. 373\u003c\/p\u003e \u003cp\u003eCHAPTER 9 SYMBOLS. 373\u003c\/p\u003e \u003cp\u003eCHAPTER 9 EQUATIONS. 373\u003c\/p\u003e \u003cp\u003eCHAPTER 9 KEY TERMS. 374\u003c\/p\u003e \u003cp\u003eCHAPTER 9 PROBLEMS. 375\u003c\/p\u003e \u003cp\u003eChapter 9 Bibliography. 380\u003c\/p\u003e \u003cp\u003e10 Slow-Speed Flight. 382\u003c\/p\u003e \u003cp\u003eRegion of Reversed Command. 383\u003c\/p\u003e \u003cp\u003eThrust producers. 384\u003c\/p\u003e \u003cp\u003ePower producers. 387\u003c\/p\u003e \u003cp\u003eStalls. 388\u003c\/p\u003e \u003cp\u003eStall Patterns. 388\u003c\/p\u003e \u003cp\u003eStall Warning Devices. 391\u003c\/p\u003e \u003cp\u003eStall Recovery. 391\u003c\/p\u003e \u003cp\u003ePower-Off Stall 393\u003c\/p\u003e \u003cp\u003ePower-On Stall 394\u003c\/p\u003e \u003cp\u003eAccelerated Stall 395\u003c\/p\u003e \u003cp\u003eCross-Control Stall 396\u003c\/p\u003e \u003cp\u003eUncoordinated Flight. 397\u003c\/p\u003e \u003cp\u003eSpins. 399\u003c\/p\u003e \u003cp\u003eSpin Warning. 399\u003c\/p\u003e \u003cp\u003eAerodynamic Characteristics of a Spin. 401\u003c\/p\u003e \u003cp\u003eImpact of Weight and Balance During a Spin. 404\u003c\/p\u003e \u003cp\u003eHazards During Slow-Speed Flight – Low-Level Wind Shear. 405\u003c\/p\u003e \u003cp\u003eAircraft Performance in Low-Level Wind Shear. 407\u003c\/p\u003e \u003cp\u003eDuring Takeoff and Departure. 407\u003c\/p\u003e \u003cp\u003eDuring Approach to a Landing. 409\u003c\/p\u003e \u003cp\u003eVertical Shear Level 410\u003c\/p\u003e \u003cp\u003eCrosswind Burst Response. 412\u003c\/p\u003e \u003cp\u003eHeavy Rain. 412\u003c\/p\u003e \u003cp\u003eHazards During Slow-Speed Flight – Turbulence. 413\u003c\/p\u003e \u003cp\u003eTurbulence Effects. 413\u003c\/p\u003e \u003cp\u003eWake Turbulence. 413\u003c\/p\u003e \u003cp\u003eMechanical Turbulence. 416\u003c\/p\u003e \u003cp\u003eConvection and Mountain Wave Turbulence. 417\u003c\/p\u003e \u003cp\u003eChapter 10 EQUATIONS. 419\u003c\/p\u003e \u003cp\u003eChapter 10 Key Terms. 419\u003c\/p\u003e \u003cp\u003eChapter 10 Problems. 420\u003c\/p\u003e \u003cp\u003eChapter 10 Bibliography. 424\u003c\/p\u003e \u003cp\u003e11 Maneuvering Performance. 426\u003c\/p\u003e \u003cp\u003eGeneral Turning Performance. 426\u003c\/p\u003e \u003cp\u003eForces in Turns. 429\u003c\/p\u003e \u003cp\u003eLoad Factor. 430\u003c\/p\u003e \u003cp\u003eLoad Factors on an Aircraft in a Coordinated Turn. 432\u003c\/p\u003e \u003cp\u003eEffect of a Coordinated Banked Turn on Stall Speed. 433\u003c\/p\u003e \u003cp\u003eThe \u003ci\u003eV\u003c\/i\u003e–\u003ci\u003eG\u003c\/i\u003e Diagram (Flight Envelope). 436\u003c\/p\u003e \u003cp\u003eManeuver Speed and Limit Load Factor. 440\u003c\/p\u003e \u003cp\u003eLoad Factor and Flight Maneuvers. 443\u003c\/p\u003e \u003cp\u003eRadius of Turn. 444\u003c\/p\u003e \u003cp\u003eRate of Turn. 448\u003c\/p\u003e \u003cp\u003eEnergy Management. 451\u003c\/p\u003e \u003cp\u003eThe Airplane as an Energy System.. 452\u003c\/p\u003e \u003cp\u003eEnergy System Control 453\u003c\/p\u003e \u003cp\u003eApplication of the Energy System.. 455\u003c\/p\u003e \u003cp\u003eCHAPTER 11 Symbols. 458\u003c\/p\u003e \u003cp\u003eCHAPTER 11 EQUATIONS. 458\u003c\/p\u003e \u003cp\u003eCHAPTER 11 KEY TERMS. 459\u003c\/p\u003e \u003cp\u003eCHAPTER 11 PROBLEMS. 460\u003c\/p\u003e \u003cp\u003eChapter 11 Bibliography. 464\u003c\/p\u003e \u003cp\u003e12 Longitudinal Stability and Control 465\u003c\/p\u003e \u003cp\u003eDefinitions. 466\u003c\/p\u003e \u003cp\u003eEquilibrium.. 466\u003c\/p\u003e \u003cp\u003eStatic Stability. 466\u003c\/p\u003e \u003cp\u003eDynamic Stability. 467\u003c\/p\u003e \u003cp\u003eOscillatory Motion. 468\u003c\/p\u003e \u003cp\u003eWeight and Balance. 469\u003c\/p\u003e \u003cp\u003eWeight and Balance Theory. 470\u003c\/p\u003e \u003cp\u003eMean Aerodynamic Chord. 472\u003c\/p\u003e \u003cp\u003eEffect of Weight on Flight Performance. 473\u003c\/p\u003e \u003cp\u003eEffect of Weight on Load Distribution. 474\u003c\/p\u003e \u003cp\u003eAirplane Reference Axes. 476\u003c\/p\u003e \u003cp\u003eStatic Longitudinal Stability. 479\u003c\/p\u003e \u003cp\u003eThe Pitching Moment Equation. 479\u003c\/p\u003e \u003cp\u003eGraphic Representation of Static Longitudinal Stability. 480\u003c\/p\u003e \u003cp\u003eContribution of Aircraft Components to Pitch Stability. 481\u003c\/p\u003e \u003cp\u003eStatic Margin and Neutral Point. 490\u003c\/p\u003e \u003cp\u003eStick-Fixed Versus Stick-Free Stability. 492\u003c\/p\u003e \u003cp\u003eAccident Brief: B-1A Static Margin Test. 492\u003c\/p\u003e \u003cp\u003eDynamic Longitudinal Stability. 494\u003c\/p\u003e \u003cp\u003ePitching Tendencies in a Stall 496\u003c\/p\u003e \u003cp\u003eLow-Tailed Aircraft. 496\u003c\/p\u003e \u003cp\u003eT-Tail Aircraft. 497\u003c\/p\u003e \u003cp\u003eExplanation of Nose-Up Pitch Following Stall in Swept-Wing Aircraft. 498\u003c\/p\u003e \u003cp\u003eLongitudinal Control 500\u003c\/p\u003e \u003cp\u003eCHAPTER 12 Symbols. 501\u003c\/p\u003e \u003cp\u003eCHAPTER 12 EQUATIONS. 502\u003c\/p\u003e \u003cp\u003eCHAPTER 12 KEY TERMS. 502\u003c\/p\u003e \u003cp\u003eCHAPTER 12 PROBLEMS. 503\u003c\/p\u003e \u003cp\u003eChapter 12 Bibliography. 507\u003c\/p\u003e \u003cp\u003e13 Directional and Lateral Stability. 509\u003c\/p\u003e \u003cp\u003eStatic Directional Stability. 509\u003c\/p\u003e \u003cp\u003eThe Yawing Moment Equation. 511\u003c\/p\u003e \u003cp\u003eGraphic Representation of Static Directional Stability. 511\u003c\/p\u003e \u003cp\u003eContribution of Aircraft Components to Yaw Stability. 512\u003c\/p\u003e \u003cp\u003eDirectional Control 517\u003c\/p\u003e \u003cp\u003eSlipstream Rotation. 517\u003c\/p\u003e \u003cp\u003eCrosswind Takeoff and Landing. 518\u003c\/p\u003e \u003cp\u003eAsymmetrical Loading\/Thrust. 518\u003c\/p\u003e \u003cp\u003eIntentional Slips. 522\u003c\/p\u003e \u003cp\u003eMulti-Engine Flight Principles. 524\u003c\/p\u003e \u003cp\u003eIntroduction to Single-Engine Flight. 525\u003c\/p\u003e \u003cp\u003eFlight Principles with One Engine Inoperative. 526\u003c\/p\u003e \u003cp\u003e\u003ci\u003eV\u003c\/i\u003eMC Considerations. 528\u003c\/p\u003e \u003cp\u003eLateral Stability and Control 531\u003c\/p\u003e \u003cp\u003eStatic Lateral Stability. 531\u003c\/p\u003e \u003cp\u003eThe Rolling Moment Equation. 533\u003c\/p\u003e \u003cp\u003eGraphic Representation of Static Lateral Stability. 533\u003c\/p\u003e \u003cp\u003eContributions of Aircraft Components to Roll Stability. 534\u003c\/p\u003e \u003cp\u003eLateral Control 539\u003c\/p\u003e \u003cp\u003eDynamic Directional and Lateral Coupled Effects. 539\u003c\/p\u003e \u003cp\u003eRoll Due to Yawing. 539\u003c\/p\u003e \u003cp\u003eAdverse Yaw.. 540\u003c\/p\u003e \u003cp\u003eTypes of Motion Resulting from Coupled Effects. 543\u003c\/p\u003e \u003cp\u003eCHAPTER 13 Symbols. 546\u003c\/p\u003e \u003cp\u003eCHAPTER 13 EQUATIONS. 547\u003c\/p\u003e \u003cp\u003eCHAPTER 13 KEY TERMS. 547\u003c\/p\u003e \u003cp\u003eCHAPTER 13 PROBLEMS. 548\u003c\/p\u003e \u003cp\u003eChapter 13 Bibliography. 551\u003c\/p\u003e \u003cp\u003e14 High-Speed Flight. 552\u003c\/p\u003e \u003cp\u003eTHE SPEED OF SOUND.. 552\u003c\/p\u003e \u003cp\u003eCoffin Corner (Q Corner). 555\u003c\/p\u003e \u003cp\u003eHIGH-SUBSONIC FLIGHT. 556\u003c\/p\u003e \u003cp\u003eNormal Shock Wave Formation on Wings. 556\u003c\/p\u003e \u003cp\u003eDESIGN FEATURES FOR HIGH-SUBSONIC FLIGHT. 557\u003c\/p\u003e \u003cp\u003eThin Airfoil Sections. 558\u003c\/p\u003e \u003cp\u003eHigh-Speed Subsonic Airfoils. 558\u003c\/p\u003e \u003cp\u003eSweepback. 559\u003c\/p\u003e \u003cp\u003eVortex Generators. 561\u003c\/p\u003e \u003cp\u003eHigh-Speed Subsonic Control Surfaces. 561\u003c\/p\u003e \u003cp\u003eFlight Control Augmentation Systems. 563\u003c\/p\u003e \u003cp\u003eTRANSONIC FLIGHT. 565\u003c\/p\u003e \u003cp\u003eWave Drag and Force Divergence. 565\u003c\/p\u003e \u003cp\u003eMach Tuck. 567\u003c\/p\u003e \u003cp\u003eHigh-Speed Mach Buffet. 569\u003c\/p\u003e \u003cp\u003eControl Surface Buzz and Flutter. 569\u003c\/p\u003e \u003cp\u003eSUPERSONIC FLIGHT. 570\u003c\/p\u003e \u003cp\u003eOblique Shock Waves. 571\u003c\/p\u003e \u003cp\u003eExpansion Waves. 572\u003c\/p\u003e \u003cp\u003eAerodynamic Forces in Supersonic Flight. 574\u003c\/p\u003e \u003cp\u003eSupersonic Airfoils. 574\u003c\/p\u003e \u003cp\u003eWing Planform.. 576\u003c\/p\u003e \u003cp\u003eArea Rule Drag Reduction. 578\u003c\/p\u003e \u003cp\u003eControl Effectiveness. 579\u003c\/p\u003e \u003cp\u003eSupersonic Engine Inlets. 581\u003c\/p\u003e \u003cp\u003eAerodynamic Heating. 584\u003c\/p\u003e \u003cp\u003eComputational Fluid Dynamics and Computer-Aided Design. 586\u003c\/p\u003e \u003cp\u003eLow Boom Flight Development. 588\u003c\/p\u003e \u003cp\u003echapter 14 SYMBOLS. 591\u003c\/p\u003e \u003cp\u003echapter 14 EQUATIONS. 591\u003c\/p\u003e \u003cp\u003echapter 14 KEY TERMS. 591\u003c\/p\u003e \u003cp\u003echapter 14 pROBLEMS. 592\u003c\/p\u003e \u003cp\u003eChapter 14 Bibliography. 595\u003c\/p\u003e \u003cp\u003e15 Rotary-Wing Flight Theory. 597\u003c\/p\u003e \u003cp\u003eMOMENTUM THEORY OF LIFT. 599\u003c\/p\u003e \u003cp\u003eAIRFOIL SELECTION.. 599\u003c\/p\u003e \u003cp\u003eFORCES ON ROTOR SYSTEM... 600\u003c\/p\u003e \u003cp\u003eTHRUST DEVELOPMENT. 603\u003c\/p\u003e \u003cp\u003eHOVERING FLIGHT. 603\u003c\/p\u003e \u003cp\u003eHovering Blade Velocity. 605\u003c\/p\u003e \u003cp\u003eBlade Twist. 605\u003c\/p\u003e \u003cp\u003eGROUND EFFECT. 605\u003c\/p\u003e \u003cp\u003eTorque. 606\u003c\/p\u003e \u003cp\u003eROTOR SYSTEMS. 608\u003c\/p\u003e \u003cp\u003eRigid Rotor. 608\u003c\/p\u003e \u003cp\u003eSemirigid Rotor (Seesaw or Teetering Hinge). 609\u003c\/p\u003e \u003cp\u003eFully Articulated Rotor. 609\u003c\/p\u003e \u003cp\u003eDISSYMMETRY OF LIFT IN FORWARD FLIGHT. 610\u003c\/p\u003e \u003cp\u003eBlade Flapping. 611\u003c\/p\u003e \u003cp\u003eBlade Lead and Lag. 612\u003c\/p\u003e \u003cp\u003eHIGH FORWARD SPEED PROBLEMS. 613\u003c\/p\u003e \u003cp\u003eAdvancing Blade Compressibility. 613\u003c\/p\u003e \u003cp\u003eRetreating Blade Stall 614\u003c\/p\u003e \u003cp\u003eGyroscopic Precession. 615\u003c\/p\u003e \u003cp\u003eHELICOPTER CONTROL. 615\u003c\/p\u003e \u003cp\u003eRotor Head Control 616\u003c\/p\u003e \u003cp\u003eControl of the Path. 617\u003c\/p\u003e \u003cp\u003eHELICOPTER POWER-REQUIRED CURVES. 617\u003c\/p\u003e \u003cp\u003eTranslational Lift. 618\u003c\/p\u003e \u003cp\u003ePOWER SETTLING, SETTLING WITH POWER, AND VORTEX RING STATE. 619\u003c\/p\u003e \u003cp\u003eAUTOROTATION.. 622\u003c\/p\u003e \u003cp\u003eDYNAMIC ROLLOVER. 624\u003c\/p\u003e \u003cp\u003eCHAPTER 15 PROBLEMS. 625\u003c\/p\u003e \u003cp\u003eCHAPTER 15 BIBLIOGRAPHY. 627\u003c\/p\u003e \u003cp\u003e16 Unmanned Aerial Vehicle Flight Theory. 628\u003c\/p\u003e \u003cp\u003eUAV Categorization. 630\u003c\/p\u003e \u003cp\u003eUAV Design. 630\u003c\/p\u003e \u003cp\u003eAerodynamics of UAV Fuselage Design. 632\u003c\/p\u003e \u003cp\u003eUAV Powerplant Design. 634\u003c\/p\u003e \u003cp\u003eThe Future of UAV Design and Aerodynamics. 640\u003c\/p\u003e \u003cp\u003eCHAPTER 16 KEY TERMS. 644\u003c\/p\u003e \u003cp\u003eCHAPTER 16 BIBLIOGRAPHY. 644\u003c\/p\u003e  \u003cp\u003e\u003cb\u003eBrian A. Johnson\u003c\/b\u003e is a former regional airline pilot, corporate pilot, and part 141 chief ground instructor. He holds an ATP with an MEL rating, commercial pilot SEL\/SES and sUAS, and currently serves as an active gold seal CFII\/MEI, full-time company pilot, and a regional FAASTeam representative. \u003c\/p\u003e\u003cp\u003e\u003cb\u003ePhilip R. Fittante\u003c\/b\u003e is a retired US Air Force Lieutenant Colonel with flight time in over 40 types of aircraft. He served as the Chief Developmental Test Pilot for the B-1B and B-2 bombers, possessing nearly 30 years of experience as an Air Force test pilot and Navy civilian test pilot and engineer.   \u003c\/p\u003e\u003cp\u003e\u003cb\u003eComprehensive introduction to aerodynamics applied to different types of modern aircraft, now updated with the latest FAA guidance\u003c\/b\u003e \u003c\/p\u003e\u003cp\u003e\u003ci\u003eFlight Theory and Aerodynamics\u003c\/i\u003e provides an introduction to aerodynamics using practical application to modern aircraft with step-by-step calculations. This fifth edition streamlines content, notably the chapters on aircraft stability, and incorporates updated FAA guidance and figures from the 2023 \u003ci\u003ePilot’s Handbook of Aeronautical Knowledge\u003c\/i\u003e as well as other FAA handbooks. \u003c\/p\u003e\u003cp\u003eA balanced application of introductory physics and meteorology in the first five chapters evolves into an introduction to propeller and jet aircraft propulsion and eventually moves into a broad discussion on the application of physics to aircraft takeoff and landing performance. After the introductory material has been presented, principles from earlier in the textbook and prior coursework are correlated and applied to slow flight, aircraft stability, and high-speed flight. A new chapter on Unmanned Aerial Vehicle (UAV) flight theory is included. \u003c\/p\u003e\u003cp\u003eThe text features extensive instructor resources including detailed PowerPoint slides for each chapter, step-by-step guidance for end of chapter calculations, sample test bank questions for each chapter, and application sections within each chapter that allow the instructor to challenge the student with additional real-world scenarios based on chapter content. \u003c\/p\u003e\u003cp\u003e\u003ci\u003eFlight Theory and Aerodynamics\u003c\/i\u003e includes information on: \u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eElements of the flight environment, covering forces, mass, scalar and vector quantities, linear and rotational motion, friction, and power\u003c\/li\u003e\n\u003cli\u003eAtmosphere, altitude, and airspeed measurement, covering properties of the atmosphere, Bernoulli’s equation, and pitot-static system advantages and disadvantages\u003c\/li\u003e\n\u003cli\u003eJet aircraft performance, covering principles of propulsion, fuel flow, specific fuel consumption, and thrust-required curves\u003c\/li\u003e\n\u003cli\u003eAircraft stability and control, covering oscillatory motion, weight and balance, and airplane reference axes\u003c\/li\u003e\n\u003cli\u003eRotary-wing flight theory, airfoil selection, and helicopter control\u003c\/li\u003e\n\u003cli\u003eUAV flight theory, including UAV design considerations, the aerodynamics of UAV fuselage design, UAV powerplant design, and the future of UAV design and aerodynamics\u003c\/li\u003e\n\u003cli\u003eEnd of chapter questions focused on scenario-based learning as applied to the performance analysis of a Diamond DA50 and corresponding chapter material.\u003c\/li\u003e\n\u003c\/ul\u003e \u003cp\u003eIn addition to degree-oriented college programs, this latest edition of \u003ci\u003eFlight Theory and Aerodynamics\u003c\/i\u003e is also an essential resource for pilot training programs ranging from student pilots to flight instructors as well as practicing professionals flying a wide range of aircraft.\u003c\/p\u003e","brand":"Wiley","offers":[{"title":"Default Title","offer_id":47989221654757,"sku":"NP9781394282296","price":136.0,"currency_code":"USD","in_stock":false}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/1842\/7735\/files\/9781394282296.jpg?v=1761783263","url":"https:\/\/k12savings.com\/es\/products\/flight-theory-and-aerodynamics-isbn-9781394282296","provider":"K12savings","version":"1.0","type":"link"}