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weathervane stability<br />

and for weathercocking tendency of aircraft on ground to<br />

face into wind. Hence * effect of vertical tail, which<br />

progressively gives directional stability to VTOL aircraft<br />

as forward speed increases.<br />

weathervane stability That provided in flight by fixed tail<br />

surfaces.<br />

weave 1 To make continuous and smooth changes of<br />

direction and height while over a period following a<br />

desired track; weaving assigned to proportion of fighters<br />

escorting slower aircraft so that continuous watch could<br />

be kept astern and in other difficult areas. Hence, weaver.<br />

2 Angular wander of spin axis, esp. of gyro, radar<br />

scanner, rotary mirror etc.<br />

WEB Web effective burn (time).<br />

web 1 Principal vertical member of a beam, spar or other<br />

primary structure running length of wing or fuselage,<br />

providing strength necessary to resist shear and keep<br />

upper and lower booms (chords) correct distance apart.<br />

Occasionally expanded to * member, * plate.<br />

2 In solid-propellant rocket, distance through which<br />

propellant burning surface will advance from initial<br />

surface until * burnout as defined by two-tanget method;<br />

usually measured as linear distance perpendicular to<br />

initial surface, symbol τ w .<br />

3 Any material form resembling sheet, either as discrete<br />

pieces or continuous * unrolled from drum or coil; esp.<br />

sheet form of prepreg, supplied in standard widths.<br />

web average burning-surface area Total volume of solid<br />

rocket propellant, excluding slivers, divided by web; thus<br />

has dimensions of an area, symbol A s .<br />

webbing Strong close-woven fabric strip produced to<br />

specified UTS, used eg for securing loose (bulk) cargo.<br />

weber, Wb SI unit of magnetic flux; that flux which,<br />

linking circuit of one turn, produces EMF of 1 V as it is<br />

reduced to zero uniformly in 1 s. Symbol Φ. To convert<br />

from maxwell, multiply by 10 –8 .<br />

web fraction Web (2) divided by internal radius of motor<br />

case or chamber; symbol f, expressed as %.<br />

web rib Rib fabricated from sheet or plate.<br />

WEC World Energy Conference.<br />

WECMC Wing electronic-combat management, or<br />

managers’, course.<br />

WECPNL Weighted equivalent continuous perceived<br />

noise level (see noise).<br />

WED Water equivalent depth.<br />

wedge 1 Air mass having wedge shape in plan, esp. such<br />

a mass of high pressure extending between two lows.<br />

2 Sharp-edged essentially 2-D * forming one wall of<br />

2-D inlet of supersonic airbreathing engine, extending<br />

ahead of inlet so that its shock may be focused on inlet lip<br />

and normally extending rearwards as a variable ramp.<br />

Hence * inlet.<br />

3 Small * added above trailing edge of aileron [rarely,<br />

other control surface] giving blunt trailing edge; supersonic<br />

equivalent of aileron cord.<br />

wedge aerofoil Sharp LE and blunt TE, useless except at<br />

supersonic speed where efficiency is high, so confined to<br />

use on missiles. See parallel double-*.<br />

WEDS Weapons effects display system.<br />

weeds, in the 1 At lowest possible level, on TFR or<br />

manually (colloq.).<br />

2 Location of [usually inadvertent] landing outside<br />

airfield boundary.<br />

weight<br />

wee-heat A simple form of on/off turbojet afterburning.<br />

weeping wing Fitted with liquid-injection leading-edge<br />

de-icing.<br />

wef, WEF With effect from.<br />

Wefax Weather facsimile format; one selectable mode<br />

of data transmission between weather satellite and ground<br />

printout.<br />

Weft Wings/engine(s)/fuselage/tail; most basic of<br />

mnemonics used in early aircraft-recognition instruction.<br />

WEG Weapons Evaluation Group (USAF).<br />

Wehnelt Type of cathode whose emissivity is enhanced<br />

by coating of radioactive-metal oxides.<br />

Weibull analysis Standardised form of plotting component<br />

failure against age, categorised as infantile, wear-out<br />

and random.<br />

Weick Coefficient for calculating propeller characteristic,<br />

also called speed/power coefficient,<br />

C s = V 5 ρ/PN 2 , where V is velocity of advance, ρ is<br />

density, P is power and N is rpm See power/speed coefficient.<br />

weighing Today almost all determination of aircraft<br />

weight is done by moving landing gears over platforms<br />

supported on load cells which measure forces by straingauges,<br />

whose output may be summed and displayed<br />

automatically. A few aircraft have landing-gear<br />

hydraulics giving a cockpit readout of weight and c.g.<br />

position.<br />

weighing points Locations, published in engineering<br />

documents and stencilled on aircraft, where jacks may be<br />

applied in weighing process.<br />

weighing record Hard copy updated each time aircraft is<br />

weighed; includes c.g. position.<br />

weigh-off Free ballooning of airship before casting off to<br />

refine trim.<br />

weight Force exerted on a mass by Earth’s gravity; thus<br />

a figure unique to a particular location which by international<br />

agreement is any at which g (free-fall acceleration)<br />

is 9.80665 m/s. For modern aeroplane some measures<br />

include: empty, complete aircraft plus systems measured<br />

in accord with specification (eg in US military usage,<br />

MIL-STD-3374); CCDR, empty minus items listed in<br />

STD-25140A such as engine(s), starter(s), electrics and<br />

avionics where removable direct from racking,<br />

wheels/brakes/tyres/tubes; standard empty, bare aircraft<br />

plus unusable fuel, full oil and full operating fluids (thus<br />

excluding potable water); basic empty, standard empty<br />

plus optional equipment; structure, bare airframe without<br />

systems and equipment other than wing/tail movables and<br />

flight-control power units, flap actuation, landing gear<br />

and actuation, and equipped engine installation(s) minus<br />

engines; useful load, those items that when added to *<br />

empty (for transport, OEW) will add up to gross weight<br />

for design mission (transport, MTOW); operating weight<br />

(military), empty plus useful load minus expendable fuel<br />

(internal/external), ammunition and stores; operating<br />

empty (OEW), equipped empty + all consumables (fuel,<br />

lube, filled galleys and bonded stocks, toiletries etc) +<br />

removable furnishings, reading and entertainment<br />

materials, cutlery, flight and cabin crews and their<br />

baggage, ship’s papers; zero-fuel (ZFW), (military) operating<br />

plus ammunition/missiles/stores, (transport)<br />

MTOW minus usable fuel; gross (military), MTOW<br />

(civil), allowable at moment of takeoff; ramp (MRW),<br />

(civil) allowable at moment of starting engines; basic<br />

772

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