Distance of stagnation point S from source in flow past half body Solution

STEP 0: Pre-Calculation Summary
Formula Used
Radial Distance = Strength of Source/(2*pi*Uniform Flow Velocity)
dradial = q/(2*pi*U)
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Radial Distance - (Measured in Meter) - Radial Distance is defined as distance between whisker sensor's pivot point to whisker-object contact point.
Strength of Source - (Measured in Square Meter per Second) - The Strength of source, q is defined as the volume flow rate per unit depth of the fluid.
Uniform Flow Velocity - (Measured in Meter per Second) - The Uniform flow velocity is considered in flow past a half body.
STEP 1: Convert Input(s) to Base Unit
Strength of Source: 1.5 Square Meter per Second --> 1.5 Square Meter per Second No Conversion Required
Uniform Flow Velocity: 9 Meter per Second --> 9 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
dradial = q/(2*pi*U) --> 1.5/(2*pi*9)
Evaluating ... ...
dradial = 0.0265258238486492
STEP 3: Convert Result to Output's Unit
0.0265258238486492 Meter --> No Conversion Required
FINAL ANSWER
0.0265258238486492 0.026526 Meter <-- Radial Distance
(Calculation completed in 00.019 seconds)

Credits

Created by Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
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Indian Institute of Technology (IIT), Bombay
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23 Incompressible Flow Characteristics Calculators

Uniform flow velocity for stream function at point in combined flow
Go Uniform Flow Velocity = (Stream Function-(Strength of Source/(2*pi*Angle A)))/(Distance from End A*sin(Angle A))
Stream Function at Point in Combined Flow
Go Stream Function = (Uniform Flow Velocity*Distance from End A*sin(Angle A))+((Strength of Source/(2*pi))*Angle A)
Location of stagnation point on x-axis
Go Distance of Stagnation Point = Distance from End A*sqrt((1+(Strength of Source/(pi*Distance from End A*Uniform Flow Velocity))))
Temperature Lapse Rate given Gas Constant
Go Temperature Lapse Rate = (-Acceleration Due to Gravity/Universal Gas Constant)*((Specific constant-1)/(Specific constant))
Stream function at point
Go Stream Function = -(Strength of Doublet/(2*pi))*(Length y/((Length X^2)+(Length y^2)))
Strength of doublet for stream function
Go Strength of Doublet = -(Stream Function*2*pi*((Length X^2)+(Length y^2)))/Length y
Uniform flow velocity for Rankine half body
Go Uniform Flow Velocity = (Strength of Source/(2*Length y))*(1-(Angle A/pi))
Dimensions of Rankine half-body
Go Length y = (Strength of Source/(2*Uniform Flow Velocity))*(1-(Angle A/pi))
Strength of source for Rankine half body
Go Strength of Source = (Length y*2*Uniform Flow Velocity)/(1-(Angle A/pi))
Pressure Head given Density
Go Pressure Head = Pressure above Atmospheric Pressure/(Density of Fluid*Acceleration Due to Gravity)
Radius of Rankine circle
Go Radius = sqrt(Strength of Doublet/(2*pi*Uniform Flow Velocity))
Pressure at point in piezometer given Mass and Volume
Go Pressure = (Mass of water*Acceleration Due to Gravity*Height of Water above Bottom of Wall)
Height of liquid in piezometer
Go Height of Liquid = Water Pressure/(Water Density*Acceleration Due to Gravity)
Distance of stagnation point S from source in flow past half body
Go Radial Distance = Strength of Source/(2*pi*Uniform Flow Velocity)
Pressure at any point in liquid
Go Pressure = Density*Acceleration Due to Gravity*Pressure Head
Stream function in sink flow for angle
Go Stream Function = (Strength of Source/(2*pi))*(Angle A)
Radius at any point considering radial velocity
Go Radius 1 = Strength of Source/(2*pi*Radial Velocity)
Radial velocity at any radius
Go Radial Velocity = Strength of Source/(2*pi*Radius 1)
Strength of source for radial velocity and at any radius
Go Strength of Source = Radial Velocity*2*pi*Radius 1
Hydrostatic law
Go Weight density = Density of Fluid*Acceleration Due to Gravity
Force on Plunger given Intensity
Go Force Acting on Plunger = Pressure Intensity*Area of plunger
Area of plunger
Go Area of plunger = Force Acting on Plunger/Pressure Intensity
Absolute Pressure given Gauge Pressure
Go Absolute Pressure = Gauge Pressure+Atmospheric Pressure

Distance of stagnation point S from source in flow past half body Formula

Radial Distance = Strength of Source/(2*pi*Uniform Flow Velocity)
dradial = q/(2*pi*U)

What is stagnation point?

In fluid dynamics, a stagnation point is a point in a flow field where the local velocity of the fluid is zero. Stagnation points exist at the surface of objects in the flow field, where the fluid is brought to rest by the object.

What is radial distance?

The radius or radial distance is the Euclidean distance from the origin O to P. The inclination (or polar angle) is the angle between the zenith direction and the line segment OP.

How to Calculate Distance of stagnation point S from source in flow past half body?

Distance of stagnation point S from source in flow past half body calculator uses Radial Distance = Strength of Source/(2*pi*Uniform Flow Velocity) to calculate the Radial Distance, The Distance of stagnation point S from source in flow past half body formula is known from the relation of stagnation point in flow past a half body considering the distance from x as 'r s' which is the radial distance. Radial Distance is denoted by dradial symbol.

How to calculate Distance of stagnation point S from source in flow past half body using this online calculator? To use this online calculator for Distance of stagnation point S from source in flow past half body, enter Strength of Source (q) & Uniform Flow Velocity (U) and hit the calculate button. Here is how the Distance of stagnation point S from source in flow past half body calculation can be explained with given input values -> 0.026526 = 1.5/(2*pi*9).

FAQ

What is Distance of stagnation point S from source in flow past half body?
The Distance of stagnation point S from source in flow past half body formula is known from the relation of stagnation point in flow past a half body considering the distance from x as 'r s' which is the radial distance and is represented as dradial = q/(2*pi*U) or Radial Distance = Strength of Source/(2*pi*Uniform Flow Velocity). The Strength of source, q is defined as the volume flow rate per unit depth of the fluid & The Uniform flow velocity is considered in flow past a half body.
How to calculate Distance of stagnation point S from source in flow past half body?
The Distance of stagnation point S from source in flow past half body formula is known from the relation of stagnation point in flow past a half body considering the distance from x as 'r s' which is the radial distance is calculated using Radial Distance = Strength of Source/(2*pi*Uniform Flow Velocity). To calculate Distance of stagnation point S from source in flow past half body, you need Strength of Source (q) & Uniform Flow Velocity (U). With our tool, you need to enter the respective value for Strength of Source & Uniform Flow Velocity 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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