Final answer:
The temperature of the air at the end of the descent will be -25.94⁰C.
Step-by-step explanation:
The temperature of the descending air can be calculated using the adiabatic lapse rate.
The adiabatic lapse rate is defined as the rate at which the temperature of a parcel of air changes as it descends or ascends without exchanging heat with its surroundings.
The adiabatic lapse rate is given by the equation:
Γ = (g / Cp) * (1 - (R / Cp))
Where:
- Γ: Adiabatic lapse rate
- g: Acceleration due to gravity (9.8 m/s²)
- Cp: Specific heat capacity at constant pressure (1004 J/kg·K)
- R: Gas constant for air (287 J/kg·K)
Substituting the values into the equation, we get:
Γ = (9.8 / 1004) * (1 - (287 / 1004)) = -0.0098 K/m
Since the air is descending, the temperature will increase at a rate of 0.0098 K/m.
The change in temperature of the parcel of air can be calculated by multiplying the lapse rate by the change in altitude:
ΔT = Γ * Δy = -0.0098 * (4267 - 1567) = -20.94 K
Therefore, the temperature of the air at the end of the descent will be:
T = -5 - 20.94 = -25.94⁰C