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stage cost<br />

two staging units; sometimes, for flight planning, one<br />

point on route.<br />

5 Various meanings in electronics, EDP (1) and other<br />

disciplines.<br />

stage cost Direct operating cost of flying one (mean, or<br />

one specific) stage (4).<br />

stage count Simple list of total number of stages of<br />

blading in fan, compressors and turbines, thus GP7200 *<br />

reads 1-5-9-2-6.<br />

staged combustion Or * combustor, fuel is supplied to<br />

groups of burners arranged in rings of different radius or<br />

in axially spaced rings or radial arms, ignited successively.<br />

staged crew Prepositioned at staging unit to take over<br />

incoming flight.<br />

stage flight One flight forming part of longer multi-stage<br />

journey.<br />

stage fuel Fuel burned in flying one stage (4); hence **<br />

carpet, plot of variables for flight-planning purposes.<br />

stage length Air-route distance between two staging<br />

points; in commercial use normally synonymous with<br />

sector distance.<br />

stage sheet Completed for each stage of maintenance<br />

listing all configuration changes and parts replaced.<br />

stage time 1 Planned or actual time at which stage (1)<br />

takes place.<br />

2 Sector time.<br />

Stagg Small turbine advanced gas-generator.<br />

stagger 1 Distance measured parallel to aircraft longitudinal<br />

axis between biplane lower-wing leading edge and<br />

vertical projection on to lower-wing extended chord line<br />

of upper-wing leading edge at same spanwise station<br />

(UK). Negative when upper plane is aft of lower.<br />

2 Acute angle measured in vertical plane parallel to<br />

aircraft longitudinal axis between leading edges of lower<br />

and upper planes at same spanwise location (US).<br />

Negative when upper plane is aft of lower.<br />

3 PRF variation by various means involving interleaving<br />

trains separated by offset interval; alternative EW<br />

technique to PRF jitter.<br />

stagger angle 1 In a biplane, the acute angle in plane<br />

parallel to aircraft longitudinal axis betwen line joining<br />

points equidistant from centreline on upper and lower LE<br />

(see stagger [1]) and local vertical.<br />

2 In a rotor blade of a gas-turbine axial compressor or<br />

turbine rotor, the angle between the principal chord at any<br />

radius and [usually] the plane through the axis of rotation;<br />

the chord line may be drawn as tangent to the LE/TE, or<br />

even through the front of the aerofoil only.<br />

stagger tuning Increasing pass-bandwidth of RF<br />

receiver by tuning different output stages (one meaning of<br />

stage [5]) slightly above or below central frequency.<br />

stagger-wing Biplane of any make with negative stagger.<br />

stagger wire Diagonal wire joining lower and upper<br />

wings of biplane and lying approximately in plane parallel<br />

to axis of symmetry. (US term; UK = incidence wire).<br />

staging 1 Separation of one stage (1) from next.<br />

2 Time at which * (1) is scheduled or actually occurs.<br />

3 Flying by separate stages (4), with or without changes<br />

of crew.<br />

staging area Geographical area between mounting area<br />

of exercise and objective, esp. for airborne or amphibious<br />

operation.<br />

staging base Landing and takeoff area with minimum<br />

servicing, supply and shelter provided for temporary<br />

stall<br />

occupancy of military aircraft during course of movement<br />

from one location to another (DoD).<br />

staging point, unit Place or organization linking two<br />

stages (4).<br />

stagnant In fluid flow, locally at rest with respect to solid<br />

containment. Avoided in most aerodynamics, and<br />

especially in fuel flow in gas-turbine injectors.<br />

stagnation line Locus joining stagnation points, eg<br />

boundary between radial-wall jets under hovering VTOL.<br />

stagnation point Point on surface of body in viscous fluid<br />

flow (one facing upstream and one down) where fluid is at<br />

rest with respect to body, flow in boundary layer on each<br />

side of ** being in opposite directions.<br />

stagnation pressure Pressure at stagnation point,<br />

normally same as total head, total pressure or pitot<br />

pressure, = sum of local atmospheric plus dynamic pressures.<br />

stagnation region Region close to upstream stagnation<br />

point.<br />

stagnation stall 1 Several related afflictions of afterburning<br />

turbofans normally occurring on afterburner<br />

light-up at high altitude at modest airspeed, in most cases<br />

with rapid pressure pulses (say, seven per second) in fan<br />

duct causing oscillating stall of fan and then core engine.<br />

2 In flight of aircraft, any stall that is not selfcorrecting.<br />

stagnation streamline That which in any representaton<br />

of 2D flow passes through front and rear stagnation<br />

points on immersed body.<br />

stagnation temperature That at stagnation point, when<br />

all relative kinetic energy has been converted isentropically<br />

to heat.<br />

stainless steel Generally, steels with 12-20 per cent<br />

chromium. Most common is 18-8, these being %<br />

chromium and nickel.<br />

Stairs Sensor technology for affordable IR systems.<br />

stair-stepped Jetpipe whose walls form a precisely calculated<br />

zigzag to minimise radar cross-section.<br />

stair-stepping Step cruising.<br />

STAJ Short-term anti-jam.<br />

stake Anvil-type bench tool for sheet.<br />

stakeholder A person or organization having a professional<br />

interest in a programme. Examples include: the<br />

customer, the customer’s advisors, and everyone<br />

concerned with the programme in the prime contractor<br />

and his suppliers and subcontractors.<br />

stake out To picket aircraft.<br />

staking Swageing terminal on to electrical conductor.<br />

Stalag Luft Prison camp for captured aircrew (G,<br />

WW2).<br />

STALD Standoff tactical air-launched decoy.<br />

stale track Shown on radar display at last known<br />

position, even though it has not appeared on susbequent<br />

updates.<br />

stall 1 Gross change in fluid flow around aerofoil,<br />

usually occurring suddenly at any 2-D section aligned<br />

with flow, at AOA just beyond limit for attached flow (at<br />

which lift coefficient is maximum); characterized by<br />

complete separation of boundary layer from upper<br />

surface and large reduction in lift. Traditional wings<br />

normally * at AOA near 16°-18°, which can be attained at<br />

any airspeed depending on applied vertical acceleration.<br />

AOA for * is increased by slat, and some highly swept<br />

650

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