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n-type for example add antimonythe are materials which have pentavalent impurity atoms donors added and conduct by the electron movement and are
questiwrite a program to find the area under the curve y fx between x a and x b integrate y fx between the limits of a and b the area under a
cold junction compensationa recent solution to the problem of controlling a reference junction temperature is to use a cold-junction compensator this
uncertainty propagationin order to calculate the error of a quantity derived from a mathematical formula which has measured variables with errors
factors affecting accuracy1 the transducer must be located in an appropriate place and with an appropriate orientation to measure the measurand
analog digital converter analog digital converter digitises the conditioned signal and presents it in a digital form which is more convenient
signal conditioning amplifierthe primary function of the signal conditioning amplifier is to match the output signal range of the transducer to
trade-offs in communications designssatellite and deep space communications - power is expensive to generate in
nomenclaturebull information source device producing information to be communicatedbull binary digit bit fundamental information unit for all digital
engineering signalsa signal is a variation of a measurable quantity that conveys information about the behaviour of a systembull a signal can depend
safe operating range the sor is the max distance between airfields which the aircraft can fly with full allowance for headwind diversion stacking
specific air range amp specific endurance key cruise parameters are range distance flown and endurance time of flight it is important to be able
maximum speed -pro craftthe standard approach for prop-driven aircraft is to assume that engine and propeller together produce a power as opposed to
wing design for a sports glider the justification of the aerofoil selection with appropriate data based on tunnel work or computational
lifting wingfp was run at the conditions corresponding to agard wg07 test case 11 namely minfin 084alpha 306 deg the lsquofinal step values of
flow at low mach number and zero incidence about m6 wingresults from fp were obtained corresponding to minfin 02 and a 0 and as noted with the
comparison of fp result with other metodscomparisons of fp results with results from other computational methods for inviscid flows are given
flow solverthe flow solver of fp utilises data produced by the grid generator together with data read from an input file named flowdat and
grid generatorthe grid generator of fp sets up a computing grid in a transform space that consists of the interior of a unit length circular
evolutionary growth approachmimic how bones plant roots add material to regions under high stress and reduce material where there is small
evolutionary methodsoptimization methods based upon natural or biological processesneed to be able to parameterise a solution and determine a cost
aerospace propulsion is essentially based on newtonslaws of motion 1687bull a body on which there is no resultant force will move ina straight line
include org 0xoo movlw 0x00 ---------- movlw 0xff movwf
control surface effectiveness and reversalto discuss the effectiveness and loss of a control surface we allow a rigid rotation delta of the flap set
torsional divergencelets first try to explain and interpret torsional divergence for the aerofoil structural model physically an additional