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endurance<br />

endurance Maximum time aircraft can continue flying<br />

under given conditions without refuelling.<br />

endurance limit Highest structural stress that permits<br />

indefinite repetition or reversal of loading; always less<br />

than yield stress (see fatigue limit).<br />

endurance on station Maximum time maritime aircraft<br />

can patrol in designated areas.<br />

ENEC Extendable nozzle exit cone.<br />

Enema Etablissement National pour l’Exploitation<br />

Météorologique et Aéronautique (Algeria).<br />

energy Capacity to do work. SI unit = joule, or [more<br />

usefully] MJ = 0.3725 hp-h, 0.277· kWh; 1 kWh =<br />

3.6000 MJ; 1hp-h = 2.68452 MJ; 1 hp-h = 2.68452 MJ; 1<br />

therm = 105.506 MJ; 1 BTU = 1.05506 kJ. At any time *<br />

of a flying vehicle is given by E h = W (h + V 2 /2 g ) where h<br />

is height above MSL and W is instantaneous mass.<br />

energy absorption test See drop test.<br />

energy conversion efficiency Ratio of kinetic energy of<br />

jet leaving nozzle to that of hypothetical ideal jet leaving<br />

ideal nozzle using same fluid under same conditions.<br />

energy density Sound energy per unit volume (usual unit<br />

is non-SI: ergs/cc).<br />

energy footprint Total area of damage caused by aircraft<br />

crashing, especially at airshow.<br />

energy height A measure of kinetic and potential energy<br />

of an air vehicle; h e = h + V 2 /2 g where h is altitude above<br />

MSL and V is TAS expressed as a velocity.<br />

energy level Any specific value of energy which a particle<br />

may adopt; during transitions from one level to another,<br />

quanta or radiant energy are emitted or absorbed,<br />

frequencies depending on difference between levels.<br />

energy management Monitoring to minimise fuel expenditure<br />

for trajectory control, navigation, environmental<br />

control, etc.<br />

energy manoeuvrability Flight manoeuvres in which full<br />

use is made of kinetic energy of aircraft, normally in<br />

trading speed for altitude.<br />

energy state Total kinetic plus potential energy<br />

possessed by aircraft, particularly a fighter; normally<br />

expressed as altitude from SL reached (without propulsion)<br />

if all such energy were converted to potential<br />

(height) energy.<br />

energy weapons See directed-energy.<br />

ENG Electronic news-gathering.<br />

Eng Engine.<br />

Engage Armed position of some arrester hooks,<br />

extended or hinged down prior to landing<br />

engage 1 In air interception, order to attack designated<br />

contact (DoD usage).<br />

2 To contact arrester wire or barrier.<br />

engage and trim indicator Panel instrument showing<br />

proper engagement of ailerons/elevators/rudder to<br />

autopilot system.<br />

engagement Encounter which involves hostile action by<br />

at least one participant.<br />

engagement control Exercised over functions of airdefence<br />

unit related to detection, identification,<br />

engagement and destruction of hostile targets.<br />

engaging speed Speed of aircraft relative to arrester wire<br />

at engagement.<br />

engin Missile (F).<br />

engine altimeter Indicates altitude corresponding to<br />

manifold pressure of supercharged engine.<br />

engine-attributable Caused by fault in an engine.<br />

enhanced GPWS<br />

engine car Airship car wholly or mainly devoted to<br />

propulsive machinery.<br />

engine change unit Aircraft piston engine removable as<br />

single unit with all accessories, cooling and oil systems.<br />

engine cowling Hinged or removable covering around<br />

aircraft engine shaped to keep drag to minimum and optimise<br />

flow of cooling air.<br />

engine critical part[s] Part[s] whose failure is likely to<br />

cause a Hazardous Engine Effect.<br />

engineered material Cellular concrete for overrun areas.<br />

engineering 1 Department responsible for detail design<br />

and development.<br />

2 Hardware design and development.<br />

engineering mock-up Full-scale replica of new aircraft or<br />

major part thereof, made [usually in metal] with<br />

high precision, partly in hard tooling, to check threedimensional<br />

geometry of structure, systems, and<br />

equipment.<br />

engineering time Number of man-hours required to<br />

complete engineering task.<br />

engineering units Pre-SI (suggested obsolete) system of<br />

units for expressing lift and drag of wing or component<br />

part in lb/sq ft at 1 mph at specified angle of attack.<br />

engine-failure recognition speed Usually written V frr .<br />

engine flight cycle The flight profile upon which the<br />

Approved Life is based.<br />

engine icing A problem with all engines, but especially<br />

with piston engine with a choke-tube carburettor, where<br />

temperature is sharply reduced.<br />

engine indication and crew alerting Eicas monitors<br />

several [typically 12] measures of engine and system<br />

performance, and can indicate impending failure.<br />

engine mounting Structure by which engine is attached<br />

to airframe.<br />

engine-out Condition in which one engine of multiengined<br />

aircraft gives no propulsive thrust.<br />

engine-plus-fuel weight A criterion of propulsive<br />

efficiency, heavy engines generally burning less fuel.<br />

engine pod See pod.<br />

engine positioner Dolly or trailer designed to carry<br />

engine, especially large turbofan, on cradle provided with<br />

hydraulic, or electrohydraulic, lateral, vertical, fore/aft,<br />

roll and pitch movement.<br />

engine pressure ratio Pressure ratio across complete<br />

compression system [possibly fan, booster and LP, IP and<br />

HP compressors]. In 1950 an axial spool of 15 stages<br />

achieved * of about 6; today this number of stages can<br />

exceed 50.<br />

engine rating Power permitted by regulations for<br />

specified use; maximum takeoff, combat, maximum<br />

continuous, weak mixture etc.<br />

engine-section stator The ring of inlet guide vanes immediately<br />

downstream of a fan at the inlet to the core.<br />

engine speed Revolutions per minute of main or other<br />

specified rotor assembly.<br />

engine swapping Replacing engines due for overhaul<br />

with stored engines that have serviceable life remaining.<br />

English bias Missile aiming error at launch, and temporary<br />

guidance commands to overcome it.<br />

EngO Pronounced N-jo, Engineer Officer (RAF).<br />

ENH Earth near horizon.<br />

enhanced GPWS Uses aircraft flight data to calculate<br />

envelope along projected flight path and compare this<br />

with internal terrain data base. Potential conflict gives<br />

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