Short Notes 04: Air Density


Basic Definitions

  • Density (ρ): Mass per unit volume of air.
  • Pressure Altitude (PA): Altitude in ISA where the observed pressure exists.
  • Density Altitude (DA): Altitude in ISA where the observed air density exists.
  • Key relationship: Aircraft performance depends on density, not pressure alone.

Gas Law Relationship

  • ρ ∝ P / T
  • Density:
    • Increases with higher pressure.
    • Decreases with higher temperature.
    • Decreases with higher humidity (moist air is lighter).

Effect of Temperature

  • Warm air → expands → lower density.
  • Cold air → contracts → higher density.
  • Warmer than ISA: DA greater than PA.
  • Colder than ISA: DA less than PA.

Effect of Pressure (Altitude)

  • Pressure decreases rapidly with height.
  • Although temperature also decreases with height, pressure decrease dominates.
  • Therefore, density always decreases with altitude.
  • At ~18,000 ft, density ≈ 50% of sea-level value.

Effect of Humidity

  • Moist air is less dense than dry air.
  • Reason:
    • Water vapour (H₂O) is lighter than N₂ and O₂.
    • Water vapour density ≈ 5/8 of dry air.
  • High humidity → higher Density Altitude → poorer performance.

Density Altitude Formula (Exam Use)

DA = PA + {ISA Deviation X times 120 }

  • ISA Deviation = OAT − ISA Temperature
  • +1°C (warmer than ISA) → DA increases by 120 ft.
  • −1°C (colder than ISA) → DA decreases by 120 ft.
  • When OAT = ISA: DA = PA.

ISA Temperature Reference

  • ISA lapse rate (for exams): 2°C / 1000 ft up to 36,090 ft.
  • Above 36,090 ft to 65,617 ft: Isothermal at −56.5°C.

Performance Implications

  • High Density Altitude (Low Density):
    • Reduced lift.
    • Reduced engine power/thrust.
    • Longer take-off distance.
    • Poor climb performance.
  • Low Density Altitude (High Density):
    • Improved aircraft and engine performance.

Lowest Density Conditions (Worst Performance)

  • Low pressure (high altitude)
  • High temperature
  • High humidity
  • Common phrase: “Hot, High, and Humid”

Highest Density Conditions (Best Performance)

  • High pressure
  • Low temperature
  • Low humidity

Moist vs Dry Air

  • At same P and T:
    • Dry air → higher density
    • Moist air → lower density

Latitude & Density (Important Concept)

  • At the surface:
    • Equator → warm → low density
    • Poles → cold → high density
  • Around ~26,000 ft: Density nearly uniform globally.
  • Above ~26,000 ft:
    • Density becomes lower at the poles than at the equator.
    • Reason: Cold polar air columns cause pressure to fall more rapidly with height.
  • Remember: Reversal of temperature–pressure–density relationship above ~8 km.

Seasonal Tropopause Note

  • Summer tropopause: Higher, colder.
  • Winter tropopause: Lower, warmer (relative comparison).

One-Line Exam Facts

  • Density Altitude = performance altitude.
  • DA equals PA only at ISA temperature.
  • Pressure change affects density more than temperature change vertically.
  • Anticyclonic (high pressure) air is denser than cyclonic air at same temperature.
  • Moist air is lighter, not heavier.

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