How to Calculate Temperature ratio at the start and end of ramming process ?
Temperature ratio at the start and end of ramming process calculator uses Temperature Ratio=1+(((Velocity^2)*(Heat Capacity Ratio-1)))/(2*(Heat Capacity Ratio*[R]*initial temp.)) to calculate the Temperature Ratio, Temperature ratio at the start and end of ramming process = 1+ (((velocity of aircraft^2) * (adiabatic_index-1))) / (2*(adiabatic_index* [R]* initial_temperature))
Here R is in Joule/Kg-K. Temperature Ratio and is denoted by T_{ratio} symbol.
How to calculate Temperature ratio at the start and end of ramming process using this online calculator? To use this online calculator for Temperature ratio at the start and end of ramming process , enter Velocity (v), initial temp. (T0) and Heat Capacity Ratio (γ) and hit the calculate button. Here is how the Temperature ratio at the start and end of ramming process calculation can be explained with given input values -> 2.948412 = 1+(((60^2)*(10-1)))/(2*(10*[R]*100)).