How to Calculate Parallel upstream flow components after shock as Mach tends to infinite?
Parallel upstream flow components after shock as Mach tends to infinite calculator uses Parallel upstream flow components =Velocity_of the fluid at 1*(1-(2*(sin(Wave angle))^2)/(Specific Heat Ratio-1)) to calculate the Parallel upstream flow components , The Parallel upstream flow components after shock as Mach tends to infinite formula is defined as the parallel component of the flow velocity after oblique shock occurs and Mach is infinite. Parallel upstream flow components and is denoted by u2 symbol.
How to calculate Parallel upstream flow components after shock as Mach tends to infinite using this online calculator? To use this online calculator for Parallel upstream flow components after shock as Mach tends to infinite, enter Velocity_of the fluid at 1 (V_{1)}, Wave angle (β) and Specific Heat Ratio (γ) and hit the calculate button. Here is how the Parallel upstream flow components after shock as Mach tends to infinite calculation can be explained with given input values -> 0.134701 = 10*(1-(2*(sin(10))^2)/(1.6-1)).