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stalled pressure<br />

(variable-sweep at max. sweep) wings exhibit no * even at<br />

AOA beyond 60°.<br />

2 Sudden breakdown in fluid flow previously attached<br />

to solid surface, caused by changed angle of either surface<br />

or flow, violent pressure pulse in flow (esp. travelling<br />

upstream) or other severe disturbance, eg flutter.<br />

3 Point at which opposing linear force or torque overcomes<br />

that of driving member (eg PFCU, hydraulic<br />

motor, airbrake or tailplane actuator), causing a<br />

commanded movement to be arrested.<br />

stalled pressure Delivery pressure at which delivery from<br />

variable-stroke fluid pump, centrifugal compressor or<br />

certain other pumps falls to zero; also called reacted<br />

pressure.<br />

stall fence Fence whose purpose is primarily to improve<br />

behaviour at stall.<br />

stalling angle AOA at which flow suddenly separates<br />

from upper surface; probably that at which C L is a<br />

maximum<br />

stalling flutter 1 Flutter in one or more degrees of<br />

freedom near angle of stall (1).<br />

2 In particular, flutter of any stalled aerofoil [eg,<br />

compressor blade] drawing energy from surrounding<br />

flow.<br />

stalling speed Any speed at which stalling AOA is<br />

reached, esp. that at 1 g when ** is at lowest value (when<br />

depends on aircraft weight, aircraft configuration and air<br />

density, among other variables). Usually assumptions<br />

include SL ISA, gear/flaps down, power off.<br />

stall-limited bank angle Maximum angle at which a coordinated<br />

turn can be sustained at maximum power, φ =<br />

cos -1 M/C Lmax S W ½ρV 2 .<br />

stall line Boundary between acceptable operating conditions<br />

for gas turbine and stall zone for any given altitude<br />

as plotted on compressor map.<br />

stall margin Difference, normally expressed as available<br />

spread of rpm, between gas-turbine operating line (at any<br />

altitude and for transient slam accelerations, etc) and stall<br />

line.<br />

stall out To stall as result of attempting too steep a climb<br />

or for any other reason, esp. when chasing opponent, thus<br />

leaving manoeuvre incomplete or failing to get into firing<br />

position.<br />

stall protection system Aeroplane flight-control<br />

subsystem sensitive to AOA (sometimes sensed at points<br />

on either side of centreline to cater for rapid-roll AOAs)<br />

which at given value triggers positive action to prevent<br />

stall; obvious example is stick-pusher, but stick-shaker is<br />

sometimes considered for inclusion.<br />

stall quality Pilot’s subjective opinion of behaviour of<br />

aircraft (normally fixed-wing aerodyne) at stall, assessed<br />

for all types of stall (eg accelerated) and configurations (eg<br />

dirty).<br />

stall recovery Urgent action to restore normal airflow<br />

over the wings. The objective is to reduce angle of attack<br />

as rapidly as possible, with minimum loss of height.<br />

Astonishingly, different methods of Standard Stall<br />

Recovery have been taught. Many authorities still insist<br />

on: Stck – Power – Pedal – Rudder if required. Today’s<br />

RAF teach: Power – Stick – forget rudder.<br />

stall strip Transverse ridge or other projection added to<br />

skin of aeroplane, usually in spanwise direction along<br />

leading edge, to serve as stall-promoter, create warning<br />

buffet and ensure stall (1) occurs first at that point.<br />

standard atmosphere<br />

stall tolerance Generally non-quantified quality of gasturbine<br />

fan and/or compressor to accept distorted airflow<br />

or other disturbance (eg gun gas, ingested jet gas, birds,<br />

hail or pressure pulses moving upstream) without stalling.<br />

stall turn Flight manoeuvre in which aircraft (aeroplane<br />

or glider) is pulled up into very steep climb, usually with<br />

engine cut well back, until on point of stall full rudder is<br />

applied to cause rapid rotation in yaw, with wings rotating<br />

in near-vertical plane; ends in dive and pullout on to<br />

desired heading (generally on to reciprocal). In US<br />

hammerhead stall (also see wingover).<br />

stall warning Anything giving pilot warning of<br />

impending stall, eg natural buffet, inbuilt ** system<br />

sensing AOA and giving visible or aural warning, or stickshaker<br />

with or without knocker.<br />

stall warning and identification system SWIS, system<br />

commanded by AOA vane (12) whose signals are analysed<br />

for AOA and rate; because of natural lag or hysteresis in<br />

system, trigger is fired progressively earlier as rate is<br />

increased by building in a phase advance giving protection<br />

at all rates.<br />

stall zone Region beyond stall line of gas turbine at any<br />

altitude where attempted pressure ratio is too great for<br />

rpm and airflow.<br />

stalo Stabilized local oscillator.<br />

Staloc Self-tracking automatic lock-on circuit.<br />

stamo Stabilized master oscillator.<br />

Stamp 1 Small tactical aerial mobility platform<br />

(USMC).<br />

2 Single-tube auto multipoint.<br />

3 Also written STAMP, Strike Air Management<br />

Programme [RN] (UK).<br />

4 Stabilized miniature payload (UAV).<br />

STAN Sum total and nose gear.<br />

Stanag, STANAG Standard NATO, or Standardization,<br />

agreement. There are hundreds, e.g., *3838<br />

repeats MIL-STD-1553B.<br />

stand 1 Place for parking one aircraft, especially at<br />

airport terminal.<br />

2 Fixed or mobile mounting for item undergoing<br />

inspection, test, maintenance or repair.<br />

stand-alone Generalized term meaning equipment, eg<br />

radar, is not integrated directly into existing system of<br />

radars or other sensors, computers and com. network.<br />

Increasingly being used for fixed-based weapon systems<br />

and even vehicle-mounted (eg airborne) equipments.<br />

Thus * ASW helicopter operates autonomously, without<br />

needing senors or other platforms.<br />

standard acceleration due to gravity See gravity.<br />

standard aerodrome “An aerodrome suitable for the<br />

operation of regular day and night services” [BS.1940].<br />

Now arch.<br />

standard air munitions package Conventional air/<br />

ground munitions required for 30-day support of one<br />

aircraft of specific type, air-transportable in three equal<br />

increments.<br />

standard atmosphere Model atmosphere defined in<br />

terms of pressure, density and temperature for all heights,<br />

assuming perfect gas, devoid of any form of water or<br />

suspended matter; approximates to real atmosphere and<br />

taken as reference for aircraft performance and all other<br />

quantitative measures. First NACA 1925 (see model<br />

atmosphere), later refined 12 times, current 1980 ICAO<br />

Doc 7488. Physical constants; P 0 10,132.5 Pa; T 0<br />

651

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