Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity Formula

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Velocity at a Point denotes the direction as well as the speed of the flow at that point. Check FAQs
V=u2(1-Cp)
V - Velocity at a Point?u - Freestream Velocity?Cp - Pressure Coefficient?

Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity Example

With values
With units
Only example

Here is how the Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity equation looks like with Values.

Here is how the Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity equation looks like with Units.

Here is how the Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity equation looks like.

47.4405Edit=110Edit2(1-0.814Edit)
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Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity Solution

Follow our step by step solution on how to calculate Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity?

FIRST Step Consider the formula
V=u2(1-Cp)
Next Step Substitute values of Variables
V=110m/s2(1-0.814)
Next Step Prepare to Evaluate
V=1102(1-0.814)
Next Step Evaluate
V=47.4404890362652m/s
LAST Step Rounding Answer
V=47.4405m/s

Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity Formula Elements

Variables
Functions
Velocity at a Point
Velocity at a Point denotes the direction as well as the speed of the flow at that point.
Symbol: V
Measurement: SpeedUnit: m/s
Note: Value can be positive or negative.
Freestream Velocity
Freestream Velocity is defined as at some distance above the boundary the velocity reaches a constant value that is free stream velocity.
Symbol: u
Measurement: SpeedUnit: m/s
Note: Value can be positive or negative.
Pressure Coefficient
Pressure Coefficient is a dimensionless parameter and it expresses the local pressure at a certain point on a surface relative to the freestream or ambient pressure.
Symbol: Cp
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
sqrt
A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
Syntax: sqrt(Number)

Other formulas in Bernoulli's Equation and Pressure Concepts category

​Go Pressure at Downstream Point by Bernoulli's Equation
P2=P1+0.5ρ0(V12-V22)
​Go Pressure at Upstream Point by Bernoulli's Equation
P1=P2-0.5ρ0(V12-V22)
​Go Static Pressure in Incompressible Flow
P1 static=P0-q1
​Go Pressure Coefficient using Velocity Ratio
Cp=1-(Vu)2

How to Evaluate Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity?

Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity evaluator uses Velocity at a Point = sqrt(Freestream Velocity^2*(1-Pressure Coefficient)) to evaluate the Velocity at a Point, Velocity at point on airfoil for given pressure coefficient and free-stream velocity formula is product of free stream velocity into square root of one minus pressure coefficient in incompressible flow. Velocity at a Point is denoted by V symbol.

How to evaluate Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity using this online evaluator? To use this online evaluator for Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity, enter Freestream Velocity (u) & Pressure Coefficient (Cp) and hit the calculate button.

FAQs on Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity

What is the formula to find Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity?
The formula of Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity is expressed as Velocity at a Point = sqrt(Freestream Velocity^2*(1-Pressure Coefficient)). Here is an example- 47.44049 = sqrt(110^2*(1-0.814)).
How to calculate Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity?
With Freestream Velocity (u) & Pressure Coefficient (Cp) we can find Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity using the formula - Velocity at a Point = sqrt(Freestream Velocity^2*(1-Pressure Coefficient)). This formula also uses Square Root (sqrt) function(s).
Can the Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity be negative?
Yes, the Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity, measured in Speed can be negative.
Which unit is used to measure Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity?
Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity 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 Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity can be measured.
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