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equator<br />

equator Primary great circle of sphere or spheroid, such<br />

as Earth, perpendicular to polar axis.<br />

equatorial bulge Excess of Earth’s equatorial diameter<br />

over polar diameter.<br />

equatorial satellite One whose orbit plane coincides, or<br />

almost coincides, with Earth’s equatorial plane.<br />

equi-axed Descriptive of traditional crystalline cast<br />

metal items.<br />

equiax blade Turbine rotor blade cast in traditional way<br />

with random arrangement of crystal axes [often capital E].<br />

equilibrium flow Fluid flow in which energy is constant<br />

along streamlines, and composition at any point is not<br />

time-dependent.<br />

equilibrium glide Hypersonic gliding flight in which sum<br />

of vertical components of aerodynamic lift and<br />

centrifugal force is equal to weight at that height.<br />

equilibrium height At which, under given conditions,<br />

equilibrium is established between lift and weight of free<br />

aerostat without power.<br />

equilibrium vapour Vapour pressure of system in which<br />

two or more phases coexist in equilibrium; in meteorology<br />

reference is to water unless otherwise specified.<br />

equinox 1 Instant that Sun occupies one equinoctial<br />

point.<br />

2 One of two points of intersection of eliptic and celestial<br />

equator, occupied by Sun when declination is 0°; also<br />

called equinoctial point.<br />

equi-period transfer orbit Orbit differing from first but<br />

having same period, eg that of lunar module following<br />

separation from command module.<br />

equipment Type or class of aircraft used or to be used on<br />

particular air-transport route(s).<br />

equipment configuration report Real-time all CMC, P/N<br />

S/N and DB/N.<br />

equipment interchange Agreement allowing aircraft to<br />

fly long routes over sectors of two or more carriers, crew<br />

being changed so that each carrier flies its own sectors.<br />

equipment operationally ready Weapon system is<br />

capable of safe use and all subsystems necessary for<br />

primary mission are ready (USAF).<br />

equipped empty weight Measured weight of individual<br />

aircraft including removable and other equipment but less<br />

disposable load.<br />

equi-signal zone Zone within which aircraft receives<br />

equal signals from left and right intersecting lobes, giving<br />

continuous on-track signal.<br />

equivalence ratio Ratio of stoichiometric to experimental<br />

air-fuel ratios.<br />

equivalent airspeed See airspeed.<br />

equivalent brake horsepower See equivalent horsepower.<br />

equivalent circuit Theoretical circuit diagram electrically<br />

equivalent to practical circuit or device.<br />

equivalent drag area See equivalent flat-plate area.<br />

equivalent flat-plate area Area of square flat plate,<br />

normal to free-stream relative airflow, which experiences<br />

same drag as the body or bodies under consideration;<br />

usually written f = D/½ρ V 2 α.<br />

equivalent flight hours 1 The equivalent actual flight time<br />

simulated in an accelerated fatigue test.<br />

2 A yardstick [C-130 EFH] established by the European<br />

Airlift Centre to enable members to trade flight time<br />

without the need to exchange funds (Int., 2004-).<br />

equivalent full-throttle power The theoretical brake<br />

horsepower which a supercharged piston engine would<br />

equivalent wing<br />

develop at sea level if it were run at full throttle and<br />

maximum r.p.m.<br />

equivalent horsepower In turboprop, sum of horsepower,<br />

usually measured as brake hp, available at<br />

propeller shaft plus equivalent power derived from jet<br />

thrust by applying numerical factor to measure of thrust<br />

(abb. ehp). See equivalent power.<br />

equivalent isotropically radiated power Product of power<br />

to antenna multiplied by antenna gain in a particular<br />

direction relative to that from isotropic antenna.<br />

equivalent kilowatt[s] SI measure of power of turboprop,<br />

abb. ekW, see equivalent power.<br />

equivalent monoplane Monoplane wing having same lift<br />

and drag properties as combination of two or more wings<br />

under consideration.<br />

equivalent monoplane aspect ratio Wings and tip vortices<br />

of biplane mutually interfere; Prandtl showed increase in<br />

induced drag of each wing is: ∆Di = ––––––––––<br />

σL 1 L 2<br />

where<br />

½ρV 2 πb 1 b 2<br />

σ is Prandtl interference factor, L wing lifts, b spans, and<br />

½ρV 2 dynamic head. Total added induced drag is twice<br />

that of single wing, so ****<br />

b 2 L<br />

O<br />

1<br />

= –––<br />

––––––––––––<br />

µ 2 (1 + r) 2<br />

where<br />

S M N µ+ 2σµr +r 2 P<br />

Q<br />

b 1 is longer span, S total area, μ ratio –––––––<br />

shorter span<br />

–––– , and<br />

longer span<br />

r ratio –––––––––––––––<br />

shorter-span lift<br />

longer-span lift<br />

equivalent pendulum Freely gimballed platform usually<br />

incorporating gyros and accelerometers, which has same<br />

period of oscillation as simple pendulum of particular<br />

length.<br />

equivalent perceived noise level LPNeq, = L E - 10 log T/t 0<br />

where L E is aircraft exposure level, T is total period of<br />

noise and t 0 is (usually) 1s (see noise).<br />

equivalent potential temperature Temperature given<br />

sample of air would have if brought adiabatically to top<br />

of atmosphere (ie to zero pressure) so that all water<br />

vapour is condensed and precipitated, remaining dry air<br />

then being compressed adiabatically to 1,000 millibars.<br />

*** is therefore determined by absolute temperature,<br />

pressure and humidity.<br />

equivalent power See equivalent horsepower; in SI units<br />

power is measured in W or multiples thereof; to a firstorder<br />

approximation ekW = kW + 68F n where F n is<br />

residual jet thrust in kN. In Imperial units jet thrust (lb<br />

force) is typically multiplied by 0.3846 [reciprocal 2.6]<br />

before being added to shaft power.<br />

equivalent shaft horsepower See equivalent horsepower.<br />

equivalent single-wheel load Mass which, supported by<br />

single wheel of size just large enough not to sink significantly<br />

into surface, causes same peak bending moment in<br />

airfield pavement as particular truck, bogie or other<br />

multi-wheel gear of actual aircraft.<br />

equivalent still-air distance The distance over the ground<br />

the aircraft would have covered in the absence of wind.<br />

equivalent temperature Temperature particle of air<br />

would have if brought adiabatically to top of atmosphere<br />

(ie to zero pressure) so that all water vapour is condensed<br />

and precipitated, remaining dry air then being compressed<br />

adiabatically to original pressure.<br />

equivalent wing In stress analysis, same span as actual<br />

wing, but with chord at each section reduced in propor-<br />

237

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