Introduction to Flight 7th Edition by John Anderson

تمرين 1

At 12 km in the standard atmosphere, the pressure, density, and temperature are 1.9399 × 10 4 N/m 2 , 3.1194 × 10 -1 kg/m 3 and 216.66 K. respectively. Using these values, calculate the standard atmospheric values of pressure, density, and temperature at an altitude of 18 km. and check with the standard altitude tables.