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Theory of Flight
6.09 Flight Instruments and Performance
Factors
References:
FTGU pages 32-34, 39-45
6.09 Flight Instruments and
Performance Factors
• MTPs:
– Pitot Static Instruments
– Asymmetric Thrust
– Precession
– Slipstream
– Climbing
– Gliding
Pitot Static Instruments
• There are three pressure instruments
– The Altimeter
– The Vertical Speed Indicator (vsi)
– The Air Speed Indicator (asi)
• There are two pressure sources
– Static Pressure
• Pressure surrounding the aircraft
– Pitot Pressure
• Pressure created by forward motion of the aircraft
• Also called dynamic pressure
Pitot Static Instruments
The Altimeter
• The Altimeter
– Operates on static
pressure
• Higher pressure 
Lower altitude
– Aneroid capsules or
wafers expand and
contract,
mechanically
moving the needles
Altimeter Markings
• Small hand reads
tens of thousands
of feet
• Medium hand reads
thousands of feet
• Large hand reads
hundreds of feet
Altimeter Errors
• Pressure Error
– Different pressures exist in different locations
– The altimeter setting compensates for changes in
pressure
• Temperature Error
– There is seldom standard temperature with a
standard lapse rate
• Mountain Effect Error
– Air is deflected around mountains
– According to Bernoulli's Principle, the pressure in the
airflow drops, which will affect the altimeter reading
The Airspeed Indicator
• Reads airspeed
(not ground
speed)
• Measures the
difference
between static
and pitot
pressure
ASI Markings
• Marked in Knots or MPH
• Red: VNE
• Yellow: Caution Range
– Highest point VNE
– Lowest point VNO
• Green: Normal Range
– Highest point VNO
– Lowest point VSL
• White: Flaps Range
– Highest point VFE
– Lowest point VSO
Some “V” Speeds
• VNE: Never Exceed Speed
• VNO: Maximum Structural Cruising Speed or
Normal Operating Limit Speed
• VSL: Power Off Stalling Speed (clean
configuration)
• VFE: Maximum Flaps Extended Speed
• VSO: Power Off Stalling Speed (flaps and
gear down)
• VA: Manoeuvring Speed
• VB: Maximum Gust Intensity Speed
ASI Errors
• Density Error
– Nonstandard pressure or alt other than 0’ASL
• Position Error
– Eddies or the angle the pitot tube meets relative
airflow
• Lag Error
– Mechanical friction
• Icing Error
– Ice covering the intake of the pressure sources
• Water Error
– Water in the system
Vertical Speed Indicator
• Reads Vertical Speed
• Measures the rate of change in static pressure
VSI Markings
• The VSI is marked in
positive and negative feet
per minute or knots of
vertical speed
VSI Errors
• Lag
– The change in altitude must occur before the
VSI can register the change
– If pitch changes are slow, the lag will be less
intense than if the pitch changes are sudden
Asymmetric Thrust
• Caused by the descending blade of the
propeller having a greater angle of attack
than the ascending blade
– High angles of attack and high power settings
• Use right rudder to compensate
Precession
• The propeller acts as a gyroscope
– Rigidity in Space
• A gyro will rotate in the same plane and resist
change
– Precession
• If forced to change, there is a tendency to rotate 90
degrees to the original axis and rotate parallel to
the applied force
• Overcome these tendencies using control
inputs as required
Slip Stream
• Air pushed backwards by the propeller has a
corkscrew pattern
– This applies force to one side of the vertical stabilizer
• Offsetting the fin, and rudder input compensates
Climbing
• Climbing changes how forces are applied
to the airplane
Climbing
• Best Angle of Climb
– Best gain for distance (by flying VX)
• Best Rate of Climb
– Best gain for time (by flying VY)
• Normal Climb
– Better engine cooling, control, and visibility over the nose
Gliding
• Gliding also changes how forces act on
the airplane
Gliding
• Gliding for Range
– Best distance covered for altitude (by flying best L/D)
• Gliding for Endurance
– Best time airborne for altitude (by flying min-sink)
Confirmation
1. What are the pitot static instruments?
2. What is another name for pitot pressure?
3. Which instrument uses pitot pressure?
4. What is the difference between VX and
VY?
5. How does a glider maintain airspeed?
CF-18 with Pilot Visible

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Flight Instruments and Performance Factor (1).ppt

  • 1. Theory of Flight 6.09 Flight Instruments and Performance Factors References: FTGU pages 32-34, 39-45
  • 2. 6.09 Flight Instruments and Performance Factors • MTPs: – Pitot Static Instruments – Asymmetric Thrust – Precession – Slipstream – Climbing – Gliding
  • 3. Pitot Static Instruments • There are three pressure instruments – The Altimeter – The Vertical Speed Indicator (vsi) – The Air Speed Indicator (asi) • There are two pressure sources – Static Pressure • Pressure surrounding the aircraft – Pitot Pressure • Pressure created by forward motion of the aircraft • Also called dynamic pressure
  • 5. The Altimeter • The Altimeter – Operates on static pressure • Higher pressure  Lower altitude – Aneroid capsules or wafers expand and contract, mechanically moving the needles
  • 6. Altimeter Markings • Small hand reads tens of thousands of feet • Medium hand reads thousands of feet • Large hand reads hundreds of feet
  • 7. Altimeter Errors • Pressure Error – Different pressures exist in different locations – The altimeter setting compensates for changes in pressure • Temperature Error – There is seldom standard temperature with a standard lapse rate • Mountain Effect Error – Air is deflected around mountains – According to Bernoulli's Principle, the pressure in the airflow drops, which will affect the altimeter reading
  • 8. The Airspeed Indicator • Reads airspeed (not ground speed) • Measures the difference between static and pitot pressure
  • 9. ASI Markings • Marked in Knots or MPH • Red: VNE • Yellow: Caution Range – Highest point VNE – Lowest point VNO • Green: Normal Range – Highest point VNO – Lowest point VSL • White: Flaps Range – Highest point VFE – Lowest point VSO
  • 10. Some “V” Speeds • VNE: Never Exceed Speed • VNO: Maximum Structural Cruising Speed or Normal Operating Limit Speed • VSL: Power Off Stalling Speed (clean configuration) • VFE: Maximum Flaps Extended Speed • VSO: Power Off Stalling Speed (flaps and gear down) • VA: Manoeuvring Speed • VB: Maximum Gust Intensity Speed
  • 11. ASI Errors • Density Error – Nonstandard pressure or alt other than 0’ASL • Position Error – Eddies or the angle the pitot tube meets relative airflow • Lag Error – Mechanical friction • Icing Error – Ice covering the intake of the pressure sources • Water Error – Water in the system
  • 12. Vertical Speed Indicator • Reads Vertical Speed • Measures the rate of change in static pressure
  • 13. VSI Markings • The VSI is marked in positive and negative feet per minute or knots of vertical speed
  • 14. VSI Errors • Lag – The change in altitude must occur before the VSI can register the change – If pitch changes are slow, the lag will be less intense than if the pitch changes are sudden
  • 15. Asymmetric Thrust • Caused by the descending blade of the propeller having a greater angle of attack than the ascending blade – High angles of attack and high power settings • Use right rudder to compensate
  • 16. Precession • The propeller acts as a gyroscope – Rigidity in Space • A gyro will rotate in the same plane and resist change – Precession • If forced to change, there is a tendency to rotate 90 degrees to the original axis and rotate parallel to the applied force • Overcome these tendencies using control inputs as required
  • 17. Slip Stream • Air pushed backwards by the propeller has a corkscrew pattern – This applies force to one side of the vertical stabilizer • Offsetting the fin, and rudder input compensates
  • 18. Climbing • Climbing changes how forces are applied to the airplane
  • 19. Climbing • Best Angle of Climb – Best gain for distance (by flying VX) • Best Rate of Climb – Best gain for time (by flying VY) • Normal Climb – Better engine cooling, control, and visibility over the nose
  • 20. Gliding • Gliding also changes how forces act on the airplane
  • 21. Gliding • Gliding for Range – Best distance covered for altitude (by flying best L/D) • Gliding for Endurance – Best time airborne for altitude (by flying min-sink)
  • 22. Confirmation 1. What are the pitot static instruments? 2. What is another name for pitot pressure? 3. Which instrument uses pitot pressure? 4. What is the difference between VX and VY? 5. How does a glider maintain airspeed?
  • 23. CF-18 with Pilot Visible