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Aerodynamics Fundamentals Overview by PeterJanuaryJazarenoGases is a document available to read on EtoBox.
What is Aerodynamics Fundamentals Overview about?
Here are the steps to solve these example problems: 1) Given: Altitude = 14000 ft, Temperature = 35°F To find: Pressure, Density 2) Use the temperature lapse rate equation: T = TO + λh 35°F = 59°F + (-0.003566°R/ft) * 14000ft 35°F = 59°F - 49.924°F Pressure = (101325 Pa) * (288 K / (288 K - 49.924 K)) ^ 5.256 Density = Pressure / (287 J/kgK * (288 K - 49.924 K)) 3) Given: Altitudes = 115
- Author
- PeterJanuaryJazarenoGases
- Language
- EN