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The Art of the Helicopter John Watkinson - Karatunov.net

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382 Index<br />

Energy and work, 29–31<br />

ki<strong>net</strong>ic energy, 30<br />

potential energy, 30<br />

Engines see Diesel piston engines/installations;<br />

Gasoline engines/installations; Turbine<br />

engines/installations<br />

Enstrom F-28, 76<br />

airframe structure, 16–17<br />

pitch control, 138–9, 140<br />

tail rotor, 175<br />

Fa 223 multi-rotor helicopter, 359–61<br />

FADEC (Full Authority Digital Engine<br />

Control), 235–7<br />

Fairey (Westland):<br />

Gyrodyne, 10, 353<br />

Rotodyne, 11, 12, 355<br />

Fatigue failure, 25<br />

Fault tolerance, 321–2<br />

electrical systems, 321–2<br />

hardover problems, 59, 321<br />

hydraulics, 321<br />

military applications, 321<br />

redundancy, 321<br />

Fea<strong>the</strong>ring, 62, 134–6<br />

cyclic fea<strong>the</strong>ring, 98<br />

Feedback, 55–60<br />

actual position, 55<br />

closed loops, 55<br />

damping/critical damping, 57<br />

desired position, 55<br />

feedback loops, 55<br />

hunting, 55–6<br />

and loop gain, 57<br />

nested loops, 57–9<br />

open loop condition, 57<br />

position error, 55<br />

with radio control <strong>of</strong> models, 59–60<br />

see also Servos<br />

Fenestron system, 167, 186–7<br />

Figure <strong>of</strong> merit, 76–7<br />

Fins, tailplane, 182–3<br />

Flameout problems, turbine engines, 235<br />

Flapback, 90<br />

tail rotors, 172<br />

Flapping, 122–3<br />

flapping bearing vibration, 100<br />

flapping bearings/hinges, 158–60, 349<br />

Gurney flap, 181<br />

tail rotor hinges, 172<br />

Flare-out and disc loading, 76<br />

Flettner Kolibri (Hummingbird), 2, 4, 198<br />

Flight directors, 262, 318<br />

see also Coupled systems<br />

Flight manuals, 339–40<br />

and operational limitations, 339–40<br />

Flight sensors:<br />

airspeed indicators (ASI), 263, 275–6, 287–8<br />

Attitude-sensing instruments, 263, 286<br />

heading sensing devices, 263<br />

height/altitude sensing indicators, 263, 276–7,<br />

325–7<br />

see also Gyroscopic instruments;<br />

Instrumentation, flying and navigation;<br />

Mag<strong>net</strong>ic compasses; Pressure instruments<br />

Flutter, rotor blades, 65–6<br />

Flux gate compass, 269–71<br />

Fly-by-wire and fly-by-light, 292<br />

Flybars:<br />

about flybars, 305<br />

see also Bell flybar system; Bell-Hiller flybar<br />

system; Hiller flybar system; Lockheed<br />

flybar system<br />

Focke-Achgelis Fa-223, 3, 5<br />

Focke-Wulf Fw-61, 2–3<br />

Following/following rate, 132<br />

Force(s):<br />

and acceleration, 22–5<br />

moments and couples, 28–9<br />

resultants and components, 26–7<br />

Forward flight:<br />

inflow and coning roll, 90–3<br />

rotor H-force, 93<br />

speed limit, 97–8<br />

tail function and design, 179<br />

tandem rotor helicopters, 370–1<br />

translational flight, 88–90<br />

Fountain effect, and ground effect, 85<br />

Fourier analysis, 46–9<br />

basic functions <strong>of</strong>, 47<br />

Heisenberg inequality, 48<br />

and helicopter rotors, 48–9<br />

inverse transforms, 47<br />

and <strong>the</strong> lift function, 98<br />

short-term Fourier transform (STFT), 48<br />

Fuel, gasoline engines, 208<br />

Fuel injection, diesel engines, 216<br />

Fuel injection, gasoline engines:<br />

basic principle, 210–11<br />

electronic systems, 211<br />

mechanical systems, 211<br />

Fuel systems:<br />

about fuel systems, 17–18<br />

air vent plumbing, 221<br />

Chinook helicopter, 222–3<br />

filtering, 221<br />

fuel type indicators, 220<br />

JetRanger helicopter, 221–2<br />

large helicopters, 221–3<br />

light helicopters, 219–21

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