v WWW.GOFLY.ONLINE Y ONLI NE FLI GHT SCHOOL CONTENTS Balance tabs.............................................................................................................................................................. 13 Mass balance............................................................................................................................................................. 13 Aileron Configurations. ...............................................................................................................................15 Differential.................................................................................................................................................................. 15 Frise........................................................................................................................................................................... 15 Flaperon..................................................................................................................................................................... 15 Manoeuvring.................................................................................................................................................15 Forces acting on an aircraft....................................................................................................................................... 15 Lift.............................................................................................................................................................................. 15 The forces in a stabilised climb..................................................................................................................17 Lift.............................................................................................................................................................................. 17 Thrust ........................................................................................................................................................................ 17 Drag .......................................................................................................................................................................... 17 The forces in a stabilised descent..............................................................................................................17 Lift.............................................................................................................................................................................. 17 Weight........................................................................................................................................................................ 17 Thrust ........................................................................................................................................................................ 17 Drag .......................................................................................................................................................................... 17 Centripetal force/G loading........................................................................................................................................ 17 Factors affecting climb performance.........................................................................................................19 Rate of climb.............................................................................................................................................................. 19 Weight........................................................................................................................................................................ 19 Power......................................................................................................................................................................... 21 Aircraft Configuration................................................................................................................................................. 21 Bank angle................................................................................................................................................................. 21 Density altitude.......................................................................................................................................................... 21 Aerodynamic Efficiency. ............................................................................................................................................ 21 Temperature............................................................................................................................................................... 21 Factors affecting descent............................................................................................................................23 Rate of descent.......................................................................................................................................................... 23 Angle of descent........................................................................................................................................................ 23 Turning..........................................................................................................................................................23 Wing Loading............................................................................................................................................................. 23 Load Factor................................................................................................................................................................ 25 Effects of bank angle...................................................................................................................................25 Stall airspeed............................................................................................................................................................. 25 Airframe..................................................................................................................................................................... 25 Limitations on steep turns. .........................................................................................................................25 Stalling, Spinning And Spiral Dives............................................................................................................25 Sloppy controls.......................................................................................................................................................... 27
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