Level 4 PC Assessment Review – Aviation
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
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
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
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
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
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
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
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