Level 4 PC Assessment Review – Aviation

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Theory of Flight

  • Boundary Layer

    • Very thin layer of air lying over the surface of the wing
    • Includes laminar and turbulent flow, which are separated by the transition point
  • Laminar flow

    • Smooth airflow over the wing
    • Initial portion until the boundary layer is tripped at the transition point
    • Laminar flow airfoils reduce the drag by maintaining the laminar flow throughout a greater percentage of the chord
  • Conventional Airfoils

    • Thickest airfoils are generally thickest at 25% of the chord
  • Aspect ratio

    • Dividing span by the average chord
  • Wash in vs wash out

    • Wash in: increasing the angle of incidence at the wing tip relative to the wing root
    • Wash out: decreasing the angle of incidence at the wing tip
  • Wing tip modifications designed to increase lift or reduce drag

    • Wing tip fuel tanks
    • Winglets
    • Drooping wing tips
  • Slots and slats

    • Slots: auxiliary airfoils that remain fixed on the leading edge
    • Slats: auxiliary airfoils that move out in front of the leading edge at high angles of attack
  • Camber

    • Curvature of the airfoil

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Instruments

  • Pitot static system
    • Pitot static system
    • Connected to the airspeed indicator, altimeter and vertical speed indicator
    • Includes a pitot pressure source and static pressure source
      • Pitot tube measures ram air pressure, or dynamic pressure, by the air rushing in due to the forward movement of the aircraft
      • Static port measures the differences in atmospheric pressure, and are not affected by ram air pressure
    • All instruments are connected to the static pressure source, where only the airspeed indicator is attached to the pitot tube
  • Airspeed Indicator errors
    • Density Error
    • Density of air depends on atmospheric pressure and temperature
    • These variables affect the air speed indicator reading as it changes the pressure differential between components within the airspeed indicator
    • Position Error
    • Depends on location of pitot tube on the aircraft
    • Farther back on the aircraft, it may receive more eddies and give a less accurate reading, where as at the front of the aircraft it is in more smooth, laminar flow
    • Lag Error
    • Mechanical error due to friction between working parts
    • Icing or Water Error
    • Blocks the pitot or static pressure sources
  • Airspeeds
    • Indicated
    • What is read off the airspeed dial
    • Calibrated
    • Indicated corrected for instrument error
    • Equivalent
    • Calibrated corrected for compressibility factor
    • True
    • Equivalent corrected for the airspeed indicator error due to density and the temperature
    • Actual speed of the airplane through the air mass
    • Mnemonic to remember airspeeds: ICE Tea is a Pretty Cool Drink
    • Moves in a zig zag pattern from I to P to C, and so on to show the different airspeeds (top row) and the factor (bottom row) that changes it to the next airspeed

I C E T

P       C       D

  • Density altitude

    • Pressure altitude corrected for temperature
  • Precession

    • Tendency of a rotating body, when a force is applied perpendicular to its plane of rotation, to turn in the direction of its rotation 90 degrees to its axis and take up a new plane of rotation parallel to the force applied.
  • Mach number

    • Mach number is calculated by dividing the airspeed by the speed of sound

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Engine

  • Fuel selector valve
    • Use to select desired fuel tank to draw fuel from
    • Use to shut off the flow of fuel from the tanks
  • Throttle
    • Forward movement opens the throttle valve, which increases the fuel to air mixture and increases the power being produced by the engine
  • Gauges
    • Oil Pressure Gauge
    • Indicates oil pressure supplied by the oil pump to lubricate the engine
    • Oil Temperature Gauge
    • Gives a reading of the temperature of the oil
    • Cylinder Head Temperature Gauge
    • Records the temperature of one or more of the engine cylinder heads
    • Gives a reasonably good indication of the effectiveness of the engine cooling system
    • Carburetor Air Temperature Gauge
    • Indicates temperature of the mixture entering the manifold
    • Or may record temperature of the intake air entering the carburetor
    • Tachometer
    • Shows the speed at which the engine crankshaft is turning in hundreds of revolutions per minute
    • Arcs:
      • Green – good
      • Yellow – caution range
      • Red – danger range
    • Manifold Pressure Gauge
    • Settings are controlled by the throttle
    • Indicates the pressure of the fuel to air mixture in the engine intake manifold between the cylinders and the carburetor
  • Pitch
    • Distance a propeller travels forward in one revolution
  • Thrust is maintained throughout most of the diameter of the propeller by means of the variation in airfoil sections and the angle of attack
  • Increase in Altitude
    • Air becomes less dense so power decreases without corrective action by the pilot

Meteorology

  • Surface friction on winds

    • Causes lower wind speeds than would be expected from the pressure gradient
    • Slows down the wind speed due to contact resistance with the ground
  • Define air mass

    • Large section of the troposphere with uniform properties of temperature, moisture within the horizontal.
  • Anabatic and katabatic winds

    • Anabatic: up slope winds flowing from valleys up the slopes to higher elevations
    • Katabatic: down slope winds flowing from high elevation down to the valleys below
    • Mnemonic: Ana ran up the hill and kicked the cat down
  • Gust

    • Rapid and irregular change of wind speed
  • Main factors determining weather in an airmass

    • Moisture content
    • Cooling process
    • Stability of the air
  • Stable air conditions

    • Stratus clouds
    • Poor visibility
    • Steady precipitation
  • Unstable air conditions

    • Cumuloform clouds
    • Good visibility
    • Showering precipitation
  • Cold Air Mass

    • More dense so sinks
    • Undercuts warmer air where will ascend over the colder air

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  • Great Circle
    • Shortest distance between two points on the surface of the earth
  • Rhumb Line
    • Lines that cuts all meridians at the same angle
    • Allows for constant direction so that the navigator may have a constant heading
  • TVMDC Headings
    • Variation is the angle between true and magnetic headings
    • Deviation is the angle between magnetic and compass headings
    • Moving from T -> M -> C add west and subtract east (east is least, west is best)
  • Isogonal Line
    • Lines drawn joining places having the same variation
  • Agonic Line
    • Joining places of zero variation
  • Compass Lead and Lag
    • ANDS – acceleration causes turns to the north, deceleration causes turns to the south
    • Occurs on east and west headings
  • Meridians of Longitude
    • Semi-great circles joining the geographical poles of the earth
    • Measured 0 to 180 degrees east and west
  • Parallels of Latitude
    • Circles in the Earth’s surface that lie parallel to the equator
    • Measured 0 to 90 degrees north and south of the equator

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