Flow Velocity Downstream of Shock Wave using Continuity Equation Solution

STEP 0: Pre-Calculation Summary
Formula Used
Velocity Downstream of Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Density Behind Normal Shock
V2 = (ρ1*V1)/ρ2
This formula uses 4 Variables
Variables Used
Velocity Downstream of Shock - (Measured in Meter per Second) - Velocity Downstream of Shock is the velocity of flow behind the shock wave.
Density Ahead of Normal Shock - (Measured in Kilogram per Cubic Meter) - Density Ahead of Normal Shock refers to the density of a fluid before encountering a normal shock wave.
Velocity Upstream of Shock - (Measured in Meter per Second) - Velocity Upstream of Shock is the velocity of flow ahead of the shock wave.
Density Behind Normal Shock - (Measured in Kilogram per Cubic Meter) - Density Behind Normal Shock represents the density of a fluid after passing through a normal shock wave.
STEP 1: Convert Input(s) to Base Unit
Density Ahead of Normal Shock: 5.4 Kilogram per Cubic Meter --> 5.4 Kilogram per Cubic Meter No Conversion Required
Velocity Upstream of Shock: 80.134 Meter per Second --> 80.134 Meter per Second No Conversion Required
Density Behind Normal Shock: 5.5 Kilogram per Cubic Meter --> 5.5 Kilogram per Cubic Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
V2 = (ρ1*V1)/ρ2 --> (5.4*80.134)/5.5
Evaluating ... ...
V2 = 78.6770181818182
STEP 3: Convert Result to Output's Unit
78.6770181818182 Meter per Second --> No Conversion Required
FINAL ANSWER
78.6770181818182 78.67702 Meter per Second <-- Velocity Downstream of Shock
(Calculation completed in 00.004 seconds)

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15 Downstream Shock Waves Calculators

Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula
Go Stagnation Pressure Behind Normal Shock = Static Pressure Ahead of Normal Shock*((1-Specific Heat Ratio+2*Specific Heat Ratio*Mach Number Ahead of Normal Shock^2)/(Specific Heat Ratio+1))*(((Specific Heat Ratio+1)^2*Mach Number Ahead of Normal Shock^2)/(4*Specific Heat Ratio*Mach Number Ahead of Normal Shock^2-2*(Specific Heat Ratio-1)))^((Specific Heat Ratio)/(Specific Heat Ratio-1))
Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number
Go Temperature Behind Normal Shock = Temperature Ahead of Normal Shock*((1+((2*Specific Heat Ratio)/(Specific Heat Ratio+1))*(Mach Number Ahead of Normal Shock^2-1))/((Specific Heat Ratio+1)*(Mach Number Ahead of Normal Shock^2)/(2+(Specific Heat Ratio-1)*Mach Number Ahead of Normal Shock^2)))
Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number
Go Enthalpy Behind Normal Shock = Enthalpy Ahead of Normal Shock*(1+((2*Specific Heat Ratio)/(Specific Heat Ratio+1))*(Mach Number Ahead of Normal Shock^2-1))/((Specific Heat Ratio+1)*(Mach Number Ahead of Normal Shock^2)/(2+(Specific Heat Ratio-1)*Mach Number Ahead of Normal Shock^2))
Mach Number behind Shock
Go Mach Number Behind Normal Shock = ((2+Specific Heat Ratio*Mach Number Ahead of Normal Shock^2-Mach Number Ahead of Normal Shock^2)/(2*Specific Heat Ratio*Mach Number Ahead of Normal Shock^2-Specific Heat Ratio+1))^(1/2)
Velocity behind Normal Shock by Normal Shock Momentum Equation
Go Velocity Downstream of Shock = sqrt((Static Pressure Ahead of Normal Shock-Static pressure Behind Normal shock+Density Ahead of Normal Shock*Velocity Upstream of Shock^2)/Density Behind Normal Shock)
Density behind Normal Shock using Normal Shock Momentum Equation
Go Density Behind Normal Shock = (Static Pressure Ahead of Normal Shock+Density Ahead of Normal Shock*Velocity Upstream of Shock^2-Static pressure Behind Normal shock)/(Velocity Downstream of Shock^2)
Static Pressure behind Normal Shock using Normal Shock Momentum Equation
Go Static pressure Behind Normal shock = Static Pressure Ahead of Normal Shock+Density Ahead of Normal Shock*Velocity Upstream of Shock^2-Density Behind Normal Shock*Velocity Downstream of Shock^2
Density behind Normal Shock given Upstream Density and Mach Number
Go Density Behind Normal Shock = Density Ahead of Normal Shock*(((Specific Heat Ratio+1)*Mach Number^2)/(2+(Specific Heat Ratio-1)*Mach Number^2))
Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number
Go Static pressure Behind Normal shock = Static Pressure Ahead of Normal Shock*(1+((2*Specific Heat Ratio)/(Specific Heat Ratio+1))*(Mach Number Ahead of Normal Shock^2-1))
Velocity behind Normal Shock from Normal Shock Energy Equation
Go Velocity Downstream of Shock = sqrt(2*(Enthalpy Ahead of Normal Shock+(Velocity Upstream of Shock^2)/2-Enthalpy Behind Normal Shock))
Velocity behind Normal Shock
Go Velocity Downstream of Shock = Velocity Upstream of Shock/((Specific Heat Ratio+1)/((Specific Heat Ratio-1)+2/(Mach Number^2)))
Enthalpy behind Normal Shock from Normal Shock Energy Equation
Go Enthalpy Behind Normal Shock = Enthalpy Ahead of Normal Shock+(Velocity Upstream of Shock^2-Velocity Downstream of Shock^2)/2
Flow Velocity Downstream of Shock Wave using Continuity Equation
Go Velocity Downstream of Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Density Behind Normal Shock
Density Downstream of Shock Wave using Continuity Equation
Go Density Behind Normal Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Velocity Downstream of Shock
Characteristic Mach Number behind Shock
Go Characteristic Mach Number Behind Shock = 1/Characteristic Mach Number Ahead of Shock

Flow Velocity Downstream of Shock Wave using Continuity Equation Formula

Velocity Downstream of Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Density Behind Normal Shock
V2 = (ρ1*V1)/ρ2

Why downstream velocity decreases across normal shock?

The velocity downstream of standing normal shock decreases because the static enthalpy increases after the normal shock and for the total enthalpy to remain constant across the normal shock, the downstream velocity decreases.

How to Calculate Flow Velocity Downstream of Shock Wave using Continuity Equation?

Flow Velocity Downstream of Shock Wave using Continuity Equation calculator uses Velocity Downstream of Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Density Behind Normal Shock to calculate the Velocity Downstream of Shock, The Flow Velocity Downstream of Shock Wave using Continuity Equation computes the velocity of a fluid downstream of a normal shock wave by applying the principle of continuity. This formula considers the density ahead of the shock, the velocity upstream of the shock, and the density behind the shock to determine the velocity downstream of the shock. Velocity Downstream of Shock is denoted by V2 symbol.

How to calculate Flow Velocity Downstream of Shock Wave using Continuity Equation using this online calculator? To use this online calculator for Flow Velocity Downstream of Shock Wave using Continuity Equation, enter Density Ahead of Normal Shock 1), Velocity Upstream of Shock (V1) & Density Behind Normal Shock 2) and hit the calculate button. Here is how the Flow Velocity Downstream of Shock Wave using Continuity Equation calculation can be explained with given input values -> 142.3636 = (5.4*80.134)/5.5.

FAQ

What is Flow Velocity Downstream of Shock Wave using Continuity Equation?
The Flow Velocity Downstream of Shock Wave using Continuity Equation computes the velocity of a fluid downstream of a normal shock wave by applying the principle of continuity. This formula considers the density ahead of the shock, the velocity upstream of the shock, and the density behind the shock to determine the velocity downstream of the shock and is represented as V2 = (ρ1*V1)/ρ2 or Velocity Downstream of Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Density Behind Normal Shock. Density Ahead of Normal Shock refers to the density of a fluid before encountering a normal shock wave, Velocity Upstream of Shock is the velocity of flow ahead of the shock wave & Density Behind Normal Shock represents the density of a fluid after passing through a normal shock wave.
How to calculate Flow Velocity Downstream of Shock Wave using Continuity Equation?
The Flow Velocity Downstream of Shock Wave using Continuity Equation computes the velocity of a fluid downstream of a normal shock wave by applying the principle of continuity. This formula considers the density ahead of the shock, the velocity upstream of the shock, and the density behind the shock to determine the velocity downstream of the shock is calculated using Velocity Downstream of Shock = (Density Ahead of Normal Shock*Velocity Upstream of Shock)/Density Behind Normal Shock. To calculate Flow Velocity Downstream of Shock Wave using Continuity Equation, you need Density Ahead of Normal Shock 1), Velocity Upstream of Shock (V1) & Density Behind Normal Shock 2). With our tool, you need to enter the respective value for Density Ahead of Normal Shock, Velocity Upstream of Shock & Density Behind Normal Shock and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Velocity Downstream of Shock?
In this formula, Velocity Downstream of Shock uses Density Ahead of Normal Shock, Velocity Upstream of Shock & Density Behind Normal Shock. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Velocity Downstream of Shock = Velocity Upstream of Shock/((Specific Heat Ratio+1)/((Specific Heat Ratio-1)+2/(Mach Number^2)))
  • Velocity Downstream of Shock = sqrt(2*(Enthalpy Ahead of Normal Shock+(Velocity Upstream of Shock^2)/2-Enthalpy Behind Normal Shock))
  • Velocity Downstream of Shock = sqrt((Static Pressure Ahead of Normal Shock-Static pressure Behind Normal shock+Density Ahead of Normal Shock*Velocity Upstream of Shock^2)/Density Behind Normal Shock)
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