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Introduction to Flight 7th Edition by John Anderson
Edition 7ISBN: 978-0073380247Introduction to Flight 7th Edition by John Anderson
Edition 7ISBN: 978-0073380247 Exercise 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.
Explanation
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For the same isothermal region with same...
Introduction to Flight 7th Edition by John Anderson
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