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Refer to the temperature distribution in the standard atmosphere as shown below. Calculate the standard atmosphere values of T, P, and ρ at a geopotential altitude of 100 meters. Use 3 decimals for the final answer and box the final answer.

Refer to the temperature distribution in the standard atmosphere as shown below. Calculate the standard atmosphere values of T, P, and ρ at a geopotential altitude of 100 meters. Use 3 decimals for the final answer and box the final answer.

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 Refer to the temperature distribution in the standard atmosphere as shown below.

Calculate the standard atmosphere values of T, P, and ρ at a geopotential altitude of 100 meters. Use 3 decimals for the final answer and box the final answer.

 

Altitude, km 100 80 60 40 20 -90 0 160 -79 165.66 K 105- 225.66 K a4 = 4 x 10-³ K/m 25- 11- 216.66 K 200 a3 = -4.5 X 10-³ K/m -47 282.66 K -53 a2 = 3 X 10-³ K/m 240 Temperature, K Figure 3.4 Temperature distribution in the standard atmosphere. a₁ = −6.5 X 10−³ K/m 288.16 K 280 320
Transcribed Image Text:Altitude, km 100 80 60 40 20 -90 0 160 -79 165.66 K 105- 225.66 K a4 = 4 x 10-³ K/m 25- 11- 216.66 K 200 a3 = -4.5 X 10-³ K/m -47 282.66 K -53 a2 = 3 X 10-³ K/m 240 Temperature, K Figure 3.4 Temperature distribution in the standard atmosphere. a₁ = −6.5 X 10−³ K/m 288.16 K 280 320
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