Find the temperature, pressure, and density at the altitude of 70 km

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September 12, 2021
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September 12, 2021

Find the temperature, pressure, and density at the altitude of 70 km

by using matlab, how can i solve this problem?8. The U.S. Standard Atmosphere specifies atmospheric properties as a function of altitude above sea level. The following table shows selected values of temperature, pressure, and density. Altitude (km) -0.5 Temperature (°C) 18.4 Pressure (atm) 1.0607 0.73702 Density (kg/m) 1.2850 0.95697 2.5 -1.1 6 -23.8 0.46589 0.66015 11 -56.2 0.22394 0.36481 20 -56.3 0.054557 0.088911 28 -48.5 50 -2.3 60 -17.2 0.015946 7.8721 X 104 2.2165 X 104 1.0227 X 10-5 1.6216 X 106 0.025076 1.0269 X 103 3.0588 X 10-4 1.9992 X 10-5 3.1703 X 106 80 -92.3 90 -92.3(a) (Matlab calculation) Draw the following three figures using Matlab. (Note: the circular dots are the data in the above table) (c) Temperature ra) 90 (6) Pressure (atmi (c) Density (kg) 90 90 80 80 80 70 70 70 60 60 60 50 50 50 Altitude (km) 40 40 40 30 30 30 20 20 20 10 10 10 0 0 o -10 -10 -10 0.0000 0.5000 10000 0.0000 0.5000 10000 15000 50 15000 -100 -50 (b) (Matlab calculation) Find the temperature, pressure, and density at the altitude of 70 km.

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