Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
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11 Other formulas that you can solve using the same Inputs

Exact Density Ratio
Density ratio=((Specific Heat Ratio+1)*((Mach Number*(sin(Wave angle)))^2))/((Specific Heat Ratio-1)*((Mach Number*(sin(Wave angle)))^2)+2) GO
Temperature ratio when Mach becomes infinite
Temperature Ratio=(2*Specific Heat Ratio*(Specific Heat Ratio-1))*((Mach Number*sin(Wave angle))^2)/(Specific Heat Ratio+1)^2 GO
Ratio of stagnation and static pressure
Stagnation to Static Pressure=(1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)))^(Specific Heat Ratio/(Specific Heat Ratio-1)) GO
Ratio of Stagnation and Static Density
Stagnation to Static Density=(1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)))^(1/(Specific Heat Ratio-1)) GO
Deflection angle
deflection angle=(2/(Specific Heat Ratio-1))*((1/Mach Number ahead of shock)-(1/Mach Number behind shock)) GO
Exact pressure ratio
pressure ratio=1+(2*Specific Heat Ratio/(Specific Heat Ratio+1))*(((Mach Number*sin(Wave angle))^2)-1) GO
Pressure ratio when Mach becomes infinite
pressure ratio=(2*Specific Heat Ratio/(Specific Heat Ratio+1))*((Mach Number*sin(Wave angle))^2) GO
Mach number
Mach Number=Fluid Velocity/(sqrt(Specific Heat Ratio*Universal Gas Constant*final temp.)) GO
Ratio of Stagnation and Static Temperature
Stagnation to Static Temperature=1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)) GO
Speed of Sound
Speed of Sound=sqrt(Specific Heat Ratio*[R-Dry-Air]*Temperature of Gas) GO
Density ratio when Mach become infinite
Density ratio=(Specific Heat Ratio+1)/(Specific Heat Ratio-1) GO

Non-dimensional perpendicular velocity component for high mach number Formula

Non dimensionalized velocity=((sin(2*Wave angle))/(Specific Heat Ratio-1))
v-=((sin(2*β))/(γ-1))
More formulas
Non-dimensional pressure GO
Non-dimensional density GO
Non-dimensional pressure for high mach number GO
Non-dimensional density for high mach number GO
Non-dimensional parallel velocity component for high mach number GO
Coefficient of pressure with slenderness ratio GO
Non dimensional radius for hypersonic vehicles GO
Transformed conical variable GO
Transformed conical variable with wave angle GO
Slenderness ratio with cone radius for hypersonic vehicle GO
Transformed conical variable with cone angle in hypersonic flow GO

What is velocity component?

The two parts of a vector are known as components and describe the influence of that vector in a single direction. If a projectile is launched at an angle to the horizontal, then the initial velocity of the projectile has both a horizontal and a vertical component

How to Calculate Non-dimensional perpendicular velocity component for high mach number?

Non-dimensional perpendicular velocity component for high mach number calculator uses Non dimensionalized velocity=((sin(2*Wave angle))/(Specific Heat Ratio-1)) to calculate the Non dimensionalized velocity, The Non-dimensional perpendicular velocity component for high mach number formula is defined as perpendicular component of the flow velocity after oblique shock occurs and Mach is infinite. Non dimensionalized velocity and is denoted by v- symbol.

How to calculate Non-dimensional perpendicular velocity component for high mach number using this online calculator? To use this online calculator for Non-dimensional perpendicular 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 perpendicular velocity component for high mach number calculation can be explained with given input values -> 1.521575 = ((sin(2*10))/(1.6-1)).

FAQ

What is Non-dimensional perpendicular velocity component for high mach number?
The Non-dimensional perpendicular velocity component for high mach number formula is defined as perpendicular component of the flow velocity after oblique shock occurs and Mach is infinite and is represented as v-=((sin(2*β))/(γ-1)) or Non dimensionalized velocity=((sin(2*Wave angle))/(Specific Heat Ratio-1)). Wave angle is the shock angle created by the oblique shock, this is not similar to the mach angle and The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.
How to calculate Non-dimensional perpendicular velocity component for high mach number?
The Non-dimensional perpendicular velocity component for high mach number formula is defined as perpendicular component of the flow velocity after oblique shock occurs and Mach is infinite is calculated using Non dimensionalized velocity=((sin(2*Wave angle))/(Specific Heat Ratio-1)). To calculate Non-dimensional perpendicular velocity component for high mach number, you need Wave angle (β) and Specific Heat Ratio (γ). With our tool, you need to enter the respective value for Wave angle and Specific Heat Ratio and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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