Static Velocity Equation using Aerodynamic Heating Equation Formula

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The Static Velocity is the speed of a fluid at a specific point in a flow field, unaffected by the motion of the surrounding fluid. Check FAQs
ue=qwρeSt(haw-hw)
ue - Static Velocity?qw - Local Heat Transfer Rate?ρe - Static Density?St - Stanton Number?haw - Adiabatic Wall Enthalpy?hw - Wall Enthalpy?

Static Velocity Equation using Aerodynamic Heating Equation Example

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With units
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Here is how the Static Velocity Equation using Aerodynamic Heating Equation equation looks like with Values.

Here is how the Static Velocity Equation using Aerodynamic Heating Equation equation looks like with Units.

Here is how the Static Velocity Equation using Aerodynamic Heating Equation equation looks like.

8.8Edit=12000Edit98.3Edit0.3059Edit(144.544Edit-99.2Edit)
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Static Velocity Equation using Aerodynamic Heating Equation Solution

Follow our step by step solution on how to calculate Static Velocity Equation using Aerodynamic Heating Equation?

FIRST Step Consider the formula
ue=qwρeSt(haw-hw)
Next Step Substitute values of Variables
ue=12000W/m²98.3kg/m³0.3059(144.544J/kg-99.2J/kg)
Next Step Prepare to Evaluate
ue=1200098.30.3059(144.544-99.2)
Next Step Evaluate
ue=8.80000651703232m/s
LAST Step Rounding Answer
ue=8.8m/s

Static Velocity Equation using Aerodynamic Heating Equation Formula Elements

Variables
Static Velocity
The Static Velocity is the speed of a fluid at a specific point in a flow field, unaffected by the motion of the surrounding fluid.
Symbol: ue
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Local Heat Transfer Rate
The Local Heat Transfer Rate is the measure of heat energy transfer per unit area at a specific location on a surface in a fluid flow.
Symbol: qw
Measurement: Heat Flux DensityUnit: W/m²
Note: Value should be greater than 0.
Static Density
The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in various mechanical and engineering applications.
Symbol: ρe
Measurement: DensityUnit: kg/m³
Note: Value should be greater than 0.
Stanton Number
The Stanton Number is a dimensionless quantity that measures the heat transfer efficiency in fluid flow over a surface, particularly in hypersonic flow scenarios.
Symbol: St
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Adiabatic Wall Enthalpy
The Adiabatic Wall Enthalpy is the heat content of a fluid in contact with an adiabatic wall, reflecting energy transfer during viscous flow conditions.
Symbol: haw
Measurement: Specific EnergyUnit: J/kg
Note: Value should be greater than 0.
Wall Enthalpy
The Wall Enthalpy is the measure of thermal energy per unit mass at the wall surface in viscous flow, influencing heat transfer and fluid behavior.
Symbol: hw
Measurement: Specific EnergyUnit: J/kg
Note: Value should be greater than 0.

Other formulas in Viscous Flow category

​Go Adiabatic Wall Enthalpy for Flat Plate
haw=he+r(h0-he)
​Go Adiabatic Wall Enthalpy using Recovery Factor
haw=he+rue22
​Go Aerodynamic Heating Equation for Stanton number
St=qwρeue(haw-hw)
​Go Coefficient of Friction using Stanton Number for Flat Plate Case
μfriction=2StPr-23

How to Evaluate Static Velocity Equation using Aerodynamic Heating Equation?

Static Velocity Equation using Aerodynamic Heating Equation evaluator uses Static Velocity = Local Heat Transfer Rate/(Static Density*Stanton Number*(Adiabatic Wall Enthalpy-Wall Enthalpy)) to evaluate the Static Velocity, Static Velocity Equation using Aerodynamic Heating Equation formula is defined as a measure of the velocity of a fluid in a flat plate for viscous flow case, taking into account the heat transfer and frictional forces, which is crucial in understanding the aerodynamic characteristics of an object. Static Velocity is denoted by ue symbol.

How to evaluate Static Velocity Equation using Aerodynamic Heating Equation using this online evaluator? To use this online evaluator for Static Velocity Equation using Aerodynamic Heating Equation, enter Local Heat Transfer Rate (qw), Static Density e), Stanton Number (St), Adiabatic Wall Enthalpy (haw) & Wall Enthalpy (hw) and hit the calculate button.

FAQs on Static Velocity Equation using Aerodynamic Heating Equation

What is the formula to find Static Velocity Equation using Aerodynamic Heating Equation?
The formula of Static Velocity Equation using Aerodynamic Heating Equation is expressed as Static Velocity = Local Heat Transfer Rate/(Static Density*Stanton Number*(Adiabatic Wall Enthalpy-Wall Enthalpy)). Here is an example- 72.34967 = 12000/(98.3*0.305932*(144.544-99.2)).
How to calculate Static Velocity Equation using Aerodynamic Heating Equation?
With Local Heat Transfer Rate (qw), Static Density e), Stanton Number (St), Adiabatic Wall Enthalpy (haw) & Wall Enthalpy (hw) we can find Static Velocity Equation using Aerodynamic Heating Equation using the formula - Static Velocity = Local Heat Transfer Rate/(Static Density*Stanton Number*(Adiabatic Wall Enthalpy-Wall Enthalpy)).
Can the Static Velocity Equation using Aerodynamic Heating Equation be negative?
No, the Static Velocity Equation using Aerodynamic Heating Equation, measured in Speed cannot be negative.
Which unit is used to measure Static Velocity Equation using Aerodynamic Heating Equation?
Static Velocity Equation using Aerodynamic Heating Equation is usually measured using the Meter per Second[m/s] for Speed. Meter per Minute[m/s], Meter per Hour[m/s], Kilometer per Hour[m/s] are the few other units in which Static Velocity Equation using Aerodynamic Heating Equation can be measured.
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