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](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fc4dacdf3-0201-4e7f-a178-d132b1817075%2F52669a7b-edc1-4929-a250-f23b9f1137ef%2F3pqign9_processed.png&w=3840&q=75)
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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