Total temperature is combination of the static temperature and velocity relation. Its SI unit is Kelvin.
Where T- static temperature
V- Velocity
Cp- specific heat at constant pressure
Category: Airplane Performance Calculator
This category helps you to calculate the airplane performance numerical like velocity, take-off distance, climb rate, turn radius, etc., – WINGS OF AERO
Total pressure is the combination of the static pressure and dynamic pressure. Its SI unit is N/m^2.
Where P- static pressure
ρ- density
V- velocity
Specific heat is the ratio of specific heat at constant pressure to the specific heat at constant volume. It is also known as Isentropic expansion factor.
Where Cp- specific heat at constant pressure
Cv- specific heat at constant volume
The Reynold number is the ratio of two forces between inertia force and viscous force. It separates the flow. It is a dimensionless quantity.
Re=ρ*V*D/μ=V*D/ν
The Reynold number is the ratio of two forces between inertia force and viscous force. It separates the flow. It is a dimensionless quantity.
Re=ρ*V*L/μ=V*L/ν