How to Calculate Non-dimensional parallel velocity component for high mach number?
Non-dimensional parallel velocity component for high mach number calculator uses Non dimensionalized upstream parallel velocity=1-((2*(sin(Wave angle))^2)/(Specific Heat Ratio-1)) to calculate the Non dimensionalized upstream parallel velocity, The Non-dimensional parallel velocity component for high mach number formula is defined as the parallel component of the flow velocity after oblique shock occurs and Mach is infinite. Non dimensionalized upstream parallel velocity and is denoted by u- symbol.
How to calculate Non-dimensional parallel velocity component for high mach number using this online calculator? To use this online calculator for Non-dimensional parallel velocity component for high mach number, enter Wave angle (β) and Specific Heat Ratio (γ) and hit the calculate button. Here is how the Non-dimensional parallel velocity component for high mach number calculation can be explained with given input values -> 0.01347 = 1-((2*(sin(10))^2)/(1.6-1)).