Total Enthalpy in Inviscid Flow Outside Boundary Layer Solution

STEP 0: Pre-Calculation Summary
Formula Used
Total Specific Enthalpy = Static Enthalpy+(Static Velocity^2)/2
h0 = he+(ue^2)/2
This formula uses 3 Variables
Variables Used
Total Specific Enthalpy - (Measured in Joule per Kilogram) - Total Specific Enthalpy defined to be the sum of the internal energy E plus the product of the pressure p and volume V.
Static Enthalpy - (Measured in Joule per Kilogram) - Static Enthalpy is the constant enthalpy of the fluid.
Static Velocity - (Measured in Meter per Second) - Static velocity is the velocity of fluid at a point in the fluid, or velocity in the continuous flow.
STEP 1: Convert Input(s) to Base Unit
Static Enthalpy: 40 Joule per Kilogram --> 40 Joule per Kilogram No Conversion Required
Static Velocity: 8.8 Meter per Second --> 8.8 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
h0 = he+(ue^2)/2 --> 40+(8.8^2)/2
Evaluating ... ...
h0 = 78.72
STEP 3: Convert Result to Output's Unit
78.72 Joule per Kilogram --> No Conversion Required
FINAL ANSWER
78.72 Joule per Kilogram <-- Total Specific Enthalpy
(Calculation completed in 00.004 seconds)

Credits

Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verified by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
Shikha Maurya has verified this Calculator and 200+ more calculators!

15 Viscous Flow Calculators

Static Velocity Equation using Aerodynamic Heating Equation
Go Static Velocity = Local Heat Transfer Rate/(Static Density*Stanton Number*(Adiabatic Wall Enthalpy-Wall Enthalpy))
Static Density Equation using Aerodynamic Equation
Go Static Density = Local Heat Transfer Rate/(Static Velocity*Stanton Number*(Adiabatic Wall Enthalpy-Wall Enthalpy))
Aerodynamic Heating Equation for Stanton number
Go Stanton Number = Local Heat Transfer Rate/(Static Density*Static Velocity*(Adiabatic Wall Enthalpy-Wall Enthalpy))
Recovery Factor using Temperature
Go Recovery Factor = (Adiabatic Wall Temperature-Static Temperature)/(Total Temperature-Static Temperature)
Recovery Factor for Flat Plate with Viscous Flow
Go Recovery Factor = (Adiabatic Wall Enthalpy-Static Enthalpy)/(Total Specific Enthalpy-Static Enthalpy)
Adiabatic Wall Enthalpy for Flat Plate
Go Adiabatic Wall Enthalpy = Static Enthalpy+Recovery Factor*(Total Specific Enthalpy-Static Enthalpy)
Drag per Unit Span
Go Drag Force = (0.86*Dynamic Pressure*Distance from Leading Edge)/sqrt(Reynolds Number)
Skin-Friction Drag Coefficient
Go Skin friction coefficient = Skin Friction Drag Force/(Dynamic Pressure*Reference Area)
Skin-Friction Drag for Flat Plate in Viscous Flow
Go Skin Friction Drag Force = Dynamic Pressure*Reference Area*Skin friction coefficient
Adiabatic Wall Enthalpy using Recovery Factor
Go Adiabatic Wall Enthalpy = Static Enthalpy+Recovery Factor*(Static Velocity^2)/2
Coefficient of Friction using Stanton Number for Flat Plate Case
Go Coefficient of Friction = (2*Stanton Number)/(Prandtl Number^(-2/3))
Stanton Number with Coefficient of Friction
Go Stanton Number = 0.5*Coefficient of Friction*Prandtl Number^(-2/3)
Total Enthalpy in Inviscid Flow Outside Boundary Layer
Go Total Specific Enthalpy = Static Enthalpy+(Static Velocity^2)/2
Recovery Factor Calculation using Prandtl Number
Go Recovery Factor = sqrt(Prandtl Number)
Prandtl Number for Flat Plate with Viscous Flow
Go Prandtl Number = Recovery Factor^2

Total Enthalpy in Inviscid Flow Outside Boundary Layer Formula

Total Specific Enthalpy = Static Enthalpy+(Static Velocity^2)/2
h0 = he+(ue^2)/2

What is enthalpy?

Enthalpy is a property of a thermodynamic system, defined as the sum of the system's internal energy and the product of its pressure and volume.

How to Calculate Total Enthalpy in Inviscid Flow Outside Boundary Layer?

Total Enthalpy in Inviscid Flow Outside Boundary Layer calculator uses Total Specific Enthalpy = Static Enthalpy+(Static Velocity^2)/2 to calculate the Total Specific Enthalpy, The Total enthalpy in inviscid flow outside boundary layer formula is defined as the function of static enthalpy, recovery factor, and static velocity. Total Specific Enthalpy is denoted by h0 symbol.

How to calculate Total Enthalpy in Inviscid Flow Outside Boundary Layer using this online calculator? To use this online calculator for Total Enthalpy in Inviscid Flow Outside Boundary Layer, enter Static Enthalpy (he) & Static Velocity (ue) and hit the calculate button. Here is how the Total Enthalpy in Inviscid Flow Outside Boundary Layer calculation can be explained with given input values -> 78.72 = 40+(8.8^2)/2.

FAQ

What is Total Enthalpy in Inviscid Flow Outside Boundary Layer?
The Total enthalpy in inviscid flow outside boundary layer formula is defined as the function of static enthalpy, recovery factor, and static velocity and is represented as h0 = he+(ue^2)/2 or Total Specific Enthalpy = Static Enthalpy+(Static Velocity^2)/2. Static Enthalpy is the constant enthalpy of the fluid & Static velocity is the velocity of fluid at a point in the fluid, or velocity in the continuous flow.
How to calculate Total Enthalpy in Inviscid Flow Outside Boundary Layer?
The Total enthalpy in inviscid flow outside boundary layer formula is defined as the function of static enthalpy, recovery factor, and static velocity is calculated using Total Specific Enthalpy = Static Enthalpy+(Static Velocity^2)/2. To calculate Total Enthalpy in Inviscid Flow Outside Boundary Layer, you need Static Enthalpy (he) & Static Velocity (ue). With our tool, you need to enter the respective value for Static Enthalpy & Static Velocity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!