
Interpretation: The stagnation temperature of the air at the given temperature and pressure is to be determined.
Concept introduction: The temperature at which a fluid is brought to rest adiabatically without any shaft work generation is called the stagnation temperature.
The stagnation temperature is given as,
The notations used here are,
Ts = Stagnation temperature
T = Air temperature
u = Speed of air
cp = Specific heat capacity
The speed of air is given as,
The notations used here are,
Ma = Mach number =
p = Pressure of the air
The density of a air is given as,
The density of air can be given as,
In the equation (3), notations used are,
P is the pressure at which air enters
M is the molecular weight of air
R is the Universal Gas constant
T is the temperature at which air enters

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Chapter 6 Solutions
Unit Operations of Chemical Engineering
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