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Airspeed Indicator and Aviation Speeds
Jul 5, 2024
Airspeed Indicator and Aviation Speeds
Overview
Discussion on airspeed indicators and aviation speeds
Divided into two videos: this part focuses on the workings, errors, and definitions of speeds
Next part: color-coded markings, reactions to pitted tube and static port blockages
Airspeed Indicator (ASI)
One of the six basic flight instruments
Connected to the pitted static system
Measures air pressure
Only instrument connected to both pitted tube (total pressure) and static port (static pressure)
Pressure Definitions
Static Pressure
: Atmospheric pressure exerted equally in all directions
Dynamic Pressure
: Pressure produced by air movement, proportional to speed and air density
Total Pressure
: Sum of static and dynamic pressure
How ASI Works
Measures dynamic pressure to indicate airspeed
Total Pressure (from pitted tube) – Static Pressure (from static port) = Dynamic Pressure
Mechanism inside ASI includes static port connected to the instrument case and pitted tube connected to a diaphragm
Diaphragm expansion/contraction moves the needle to indicate speed
Errors and Corrections
Indicated Airspeed (IAS)
: Speed indicated on the instrument, not corrected for errors
Instrument Error
: Due to manufacturing imperfections and wear
Position Error
: Changes in flaps, gear, and maneuvers
Calibrated Airspeed (CAS)
: IAS corrected for instrument and position errors
Determined using calibration tables from aircraft manual
Compressibility Error
: Air compresses at high speeds (>300 knots), not considered in small aircraft
Equivalent Airspeed (EAS)
: CAS corrected for compressibility errors
Density Error
: Related to air density, affects dynamic pressure and thus airspeed
True Airspeed (TAS)
: EAS corrected for density error, reflects actual speed relative to the air
Calculated using formula or flight computer
Ground Speed (GS)
: TAS corrected by wind effects, actual speed relative to the ground
Tailwind increases GS, headwind decreases GS
Summary of Speed Terms
IAS
: Direct reading from airspeed indicator
CAS
: IAS + corrections for instrument/position errors
EAS
: CAS + corrections for compressibility errors
TAS
: EAS + corrections for density errors
GS
: TAS + wind correction
Practical Applications
IAS
: Structural limitations, take-off/landing speeds, stall speeds, performance speeds
TAS
: ATC flight plans, Mach speed, endurance, wind correction, flight planning
GS
: Flight time, fuel consumption, climb/descent parameters, general flight planning
Conclusion
Understanding each speed is crucial for various flight operations
Some aircraft have automated systems to handle these calculations
Importance of practical knowledge for day-to-day flight operations
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