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centimetric radar<br />

centimetric radar Radar operating on wavelengths<br />

around 0.01 m, with frequencies 3–30 GHz.<br />

centipoise See viscosity.<br />

centistoke See viscosity.<br />

CENTO, Cento Central Treaty Organization (1955–80,<br />

Iran, Iraq, Pakistan, Turkey, UK, US).<br />

central altitude reservation See CARF.<br />

centralised fault display system Avionics system<br />

accessing all on-board BITE systems to extract and<br />

display data and initiate maintenance tests.<br />

centralised servicing Establishment of one unit and site<br />

for all routine maintenance on station, breaking previous<br />

intimate relationship between crew chief and each aircraft<br />

(RAF).<br />

central warning panel See CWP (I).<br />

centrebody Streamlined body in centre of circular, semicircular<br />

or quasi-circular supersonic intake (inlet) to cause<br />

inclined shock.<br />

centre controls To move primary flight controls from<br />

deflected to neutral position.<br />

centre engine Engine on centreline of multi-engined<br />

aircraft.<br />

centreline 1 Principal longitudinal axis; usually also axis<br />

of symmetry (eg of aircraft, missile, runway).<br />

2 In aerofoil section, line joining leading and trailing<br />

edges and everywhere equidistant from upper and lower<br />

surfaces, all measures being normal to line itself.<br />

centreline aircraft See centreline engine[s].<br />

centreline camber Ratio of maximum distance between<br />

chord and centreline (2) to chord.<br />

centreline closure Compressor, or [more often] turbineblade<br />

rub caused by slight radial displacement.<br />

centreline engine[s] Any engine on longitudinal centreline<br />

of multi-engine aircraft [engines hung on side of<br />

fuselage or in wing roots are excluded]. The pilot does not<br />

need a multi-engine rating.<br />

centreline gear Main landing gear on aircraft centreline.<br />

centreline lighting On runway, flush lights at 50 ft (15 m)<br />

intervals terminating 75 ft (23 m) from each threshold.<br />

centreline noise plot Plot of aircraft noise, usually<br />

EPNdB, along runway centreline extended (usually 6 st<br />

miles, 9.6 km) in each direction covering approach and<br />

climb-out.<br />

centreline tank Centre tank 1 [not 2].<br />

centre of area See centroid.<br />

centre of buoyancy Point through which upthrust of<br />

displaced fluid acts; e.g. in case of aerostats and marine<br />

aircraft afloat.<br />

centre of burst Mean point of impact.<br />

centre of dynamic lift In aerostat, point on centreline<br />

through which lift force due to motion through atmosphere<br />

acts.<br />

centre of gravity, c.g. Point through which resultant<br />

force of gravity acts, irrespective of orientation; in<br />

uniform gravitational field, centre of mass. For twodimensional<br />

forms, centroid.<br />

centre of gravity limits In nearly all aircraft, esp. aerodynes,<br />

published fore and aft limits for safe c.g. position;<br />

in case of aeroplanes expressed as percentages of MAC.<br />

centre of gravity margin H n , distance along aircraft<br />

major axis from c.g. to neutral point, expressed as<br />

% SMC.<br />

centre of gravity travel Fore and aft wander of c.g. in<br />

centrifugal compressor<br />

course of flight due to consumption of fuel, release of<br />

loads, etc.<br />

centre of gross lift In aerostat, usually centre of buoyancy.<br />

centre of gyration For solid rotating about axis, point at<br />

which all mass could be concentrated without changing<br />

moment of inertia about same axis.<br />

centre of lift Resultant of all centres of pressure on a<br />

wing or other body.<br />

centre of mass Point through which all mass of solid<br />

body could act without changing dynamics in translational<br />

motion; loosely, but not always correctly, called<br />

c.g. Alternative title, centre of inertia.<br />

centre of pressure, c.p. On aerofoil, point at which line<br />

of action of resultant aerodynamic force intersects chord.<br />

Almost same as aerodynamic centre, but latter need not<br />

lie on chord. In general, c.p. is resultant of all aerodynamic<br />

forces on surface of body.<br />

centre of pressure coefficient Ratio of distance of c.p.<br />

from leading edge to chord.<br />

centre of pressure moment Product of resultant force on<br />

wing (or section) and distance from c.p. to leading edge<br />

(or leading edge produced at aircraft centreline).<br />

Inapplicable to very slender wings.<br />

centre of pressure moment coefficient As above but<br />

divided by dynamic pressure; not same as coefficient of<br />

moment.<br />

centre of pressure travel 1 Linear distance through<br />

which c.p. travels along chord over extreme negative to<br />

positive operating range of angles of attack, ignoring<br />

compressibility in subsonic flow.<br />

2 Linear distance through which c.p. travels along<br />

chord over complete aircraft operating range of Mach<br />

numbers (supersonic aircraft only).<br />

centre of thrust Thrust axis, for one or multiple engines.<br />

centre of twist The axis about which a solid body rotates<br />

when under an applied torque.<br />

centre punch Hand tool for making accurate conical<br />

depressions.<br />

centre section In most winged aircraft, centre portion of<br />

wing extending symmetrically through or across fuselage<br />

and carrying left and right wings on its tips. Certain<br />

aircraft have wing in one piece, or in left and right halves<br />

joined at centreline; such have no **, though some authorities<br />

suggest it is then wing inboard of main landing gear.<br />

centre tank 1 Most commonly, a fuel tank inside the<br />

fuselage in a system havng additional tanks in the wings.<br />

2 A tank inside the inboard part of each wing, usually<br />

structurally part of the single main inter-spar box, and<br />

separated from the main tank by a rib.<br />

centrifugal breather Centrifuge filter for removing oil<br />

from air vented overboard from interior of engine, often<br />

after passage through porous segments.<br />

centrifugal clearance Radial clearance between rotating<br />

mass and surrounding fixed structure at peak rotating<br />

speed.<br />

centrifugal clutch Freewheels at low speed, but takes up<br />

drive as speed is increased. At full power slip tends<br />

towards zero. Main purpose is to prevent excessive load<br />

on gearteeth.<br />

centrifugal compressor Rotary compressor in form of<br />

disc carrying radial vanes to accelerate working fluid radially<br />

outward to leave periphery at very high speed, this<br />

being converted to pressure energy in fixed diffuser.<br />

135

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