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.
