Shikha Maurya
Indian Institute of Technology (IIT), Bombay
Shikha Maurya has created this Calculator and 100+ more calculators!
Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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11 Other formulas that you can solve using the same Inputs

Velocity ahead of normal shock by normal shock momentum equation
Velocity upstream of shock=sqrt(((Static pressure behind shock-(Static pressure ahead of shock)+(Density behind shock*Velocity downstream of shock^2))/density ahead of shock)) GO
Static Pressure behind of normal shock using normal shock momentum equation
Static pressure behind shock=Static pressure ahead of shock+(density ahead of shock*(Velocity upstream of shock^2))-(Density behind shock*(Velocity downstream of shock^2)) GO
Velocity behind of normal shock by normal shock momentum equation
Velocity downstream of shock=sqrt((Static pressure ahead of shock-Static pressure behind shock+(density ahead of shock*(Velocity upstream of shock^2)))/Density behind shock) GO
Static Pressure ahead of normal shock using normal shock momentum equation
Static pressure ahead of shock=Static pressure behind shock+(Density behind shock*(Velocity downstream of shock^2))-(density ahead of shock*(Velocity upstream of shock^2)) GO
Density ahead of normal shock using normal shock momentum equation
density ahead of shock=(Static pressure behind shock+(Density behind shock*(Velocity downstream of shock^2))-Static pressure ahead of shock)/(Velocity upstream of shock^2) GO
Density behind normal shock using normal shock momentum equation
Density behind shock=(Static pressure ahead of shock+(density ahead of shock*(Velocity upstream of shock^2))-Static pressure behind shock)/(Velocity downstream of shock^2) GO
Velocity behind a normal shock
Velocity downstream of shock=Velocity upstream of shock/((Specific heat ratio+1)/((Specific heat ratio-1)+(2/(Mach Number ahead of shock^2)))) GO
Velocity behind of normal shock from normal shock energy equation
Velocity downstream of shock=sqrt(2*(Enthalpy ahead shock+((Velocity upstream of shock^2)/2)-Enthalpy behind shock)) GO
Velocity ahead of normal shock from normal shock energy equation
Velocity upstream of shock=sqrt(2*(Enthalpy behind shock+((Velocity downstream of shock^2)/2)-Enthalpy ahead shock)) GO
Enthalpy behind of normal shock from normal shock energy equation
Enthalpy behind shock=Enthalpy ahead shock+((Velocity upstream of shock^2)-(Velocity downstream of shock^2))/2 GO
Prandtl Condition
Velocity downstream of shock=(Critical speed of sound^2)/Velocity upstream of shock GO

Enthalpy ahead of normal shock from normal shock energy equation Formula

Enthalpy ahead shock=Enthalpy behind shock+((Velocity downstream of shock^2)-(Velocity upstream of shock^2))/2
h<sub>1</sub>=h<sub>2</sub>+((V<sub>2</sub>^2)-(V<sub>1</sub>^2))/2
More formulas
Prandtl Condition GO
Characteristic Mach Number behind shock GO
Characteristic Mach number GO
Relation between Characteristic Mach number and Mach number GO
Mach Number behind the shock GO
Shock strength GO
Velocity behind a normal shock GO
Entropy change across normal shock GO
Static Pressure ahead of normal shock using normal shock momentum equation GO
Static Pressure behind of normal shock using normal shock momentum equation GO
Density ahead of normal shock using normal shock momentum equation GO
Density behind normal shock using normal shock momentum equation GO
Enthalpy behind of normal shock from normal shock energy equation GO
Velocity ahead of normal shock from normal shock energy equation GO
Velocity behind of normal shock from normal shock energy equation GO
Velocity behind of normal shock by normal shock momentum equation GO
Velocity ahead of normal shock by normal shock momentum equation GO
Velocity upstream of shock using Prandtl relation GO
Critical speed of sound from Prandtl relation GO
Density ratio across a normal shock GO
Pressure ratio across a normal shock GO
Temperature ratio across a normal shock GO
Static enthalpy ratio across a normal shock GO
Stagnation pressure behind normal shock by Rayleigh Pitot tube formula GO
Density behind normal shock for given upstream density and Mach number GO
Static pressure behind normal shock for given upstream pressure and Mach number GO
Static temperature behind normal shock for given upstream temperature and Mach number GO
Static enthalpy behind normal shock for given upstream enthalpy and Mach number GO

What is total enthalpy?

At any point in a flow, the total enthalpy is given by the sum of the static enthalpy plus the kinetic energy, all per unit mass.

What is static enthalpy?

Static enthalpy is defined as the sum of the system's internal energy and the product of its pressure and volume. Static enthalpy changes before and after the normal shock.

How to Calculate Enthalpy ahead of normal shock from normal shock energy equation?

Enthalpy ahead of normal shock from normal shock energy equation calculator uses Enthalpy ahead shock=Enthalpy behind shock+((Velocity downstream of shock^2)-(Velocity upstream of shock^2))/2 to calculate the Enthalpy ahead shock, The Enthalpy ahead of normal shock from normal shock energy equation formula is defined as the sum of downstream static enthalpy plus the half of the square of the downstream velocity after shock and then subtracting the half of the square of the upstream velocity of fluid ahead of the shock. Enthalpy ahead shock and is denoted by h1 symbol.

How to calculate Enthalpy ahead of normal shock from normal shock energy equation using this online calculator? To use this online calculator for Enthalpy ahead of normal shock from normal shock energy equation, enter Enthalpy behind shock (h2), Velocity downstream of shock (V2) and Velocity upstream of shock (V1) and hit the calculate button. Here is how the Enthalpy ahead of normal shock from normal shock energy equation calculation can be explained with given input values -> -3703 = 47+((50^2)-(100^2))/2.

FAQ

What is Enthalpy ahead of normal shock from normal shock energy equation?
The Enthalpy ahead of normal shock from normal shock energy equation formula is defined as the sum of downstream static enthalpy plus the half of the square of the downstream velocity after shock and then subtracting the half of the square of the upstream velocity of fluid ahead of the shock and is represented as h1=h2+((V2^2)-(V1^2))/2 or Enthalpy ahead shock=Enthalpy behind shock+((Velocity downstream of shock^2)-(Velocity upstream of shock^2))/2. Enthalpy behind shock is the enthalpy of downstream of shock and it is defined as the sum of the system's internal energy and the product of its pressure and volume for per unit mass, Velocity downstream of shock is the velocity of flow behind the shock wave and Velocity upstream of shock is the velocity of flow ahead of the shock wave.
How to calculate Enthalpy ahead of normal shock from normal shock energy equation?
The Enthalpy ahead of normal shock from normal shock energy equation formula is defined as the sum of downstream static enthalpy plus the half of the square of the downstream velocity after shock and then subtracting the half of the square of the upstream velocity of fluid ahead of the shock is calculated using Enthalpy ahead shock=Enthalpy behind shock+((Velocity downstream of shock^2)-(Velocity upstream of shock^2))/2. To calculate Enthalpy ahead of normal shock from normal shock energy equation, you need Enthalpy behind shock (h2), Velocity downstream of shock (V2) and Velocity upstream of shock (V1). With our tool, you need to enter the respective value for Enthalpy behind shock, Velocity downstream of shock and Velocity upstream of shock 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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