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Instantaneous flow per section

Storyboard

>Model

ID:(2070, 0)



Mechanisms

Iframe

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Code
Concept

Mechanisms

ID:(15713, 0)



Instant Volume Flow

Concept

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The definition of the volume flow (J_V) is the volume element (\Delta V) over the time elapsed (\Delta t):

J_V =\displaystyle\frac{ \Delta V }{ \Delta t }



which, in the limit of an infinitesimal time interval, corresponds to the derivative of the volume (V) with respect to the time (t):

J_V =\displaystyle\frac{ dV }{ dt }

ID:(15718, 0)



Volume Flow and its Speed

Concept

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The volume (V) for a tube with constant the section Tube (S) and a position (s) is

V = s S



If the section Tube (S) is constant, the temporal derivative will be

\displaystyle\frac{dV}{dt} = S\displaystyle\frac{ds}{dt}



thus, with the volume flow (J_V) defined by

J_V =\displaystyle\frac{ dV }{ dt }



and with the flux density (j_s) associated with the position (s) via

j_s =\displaystyle\frac{ ds }{ dt }



it is concluded that

J_V = S j_s

ID:(15717, 0)



Flow for inhomogeneous flux density

Concept

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In the case that the flux density (j_s) is constant, the volume flow (J_V) can be calculated using the section or Area (S) according to:

J_V = S j_s



If the flux density (j_s) varies, sufficiently small sectional elements dS can be considered so that the equation remains valid in the sense that the contribution to flow is:

dJ_V = j_s dS



Integrating this expression over the entire section results in

J_V =\displaystyle\int j_s dS

ID:(15719, 0)



Model

Top

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Parameters

Symbol
Text
Variable
Value
Units
Calculate
MKS Value
MKS Units
V
V
Volumen
m^3

Variables

Symbol
Text
Variable
Value
Units
Calculate
MKS Value
MKS Units
j_s
j_s
Flux density
m/s
s
s
Position
m
S_d
S_d
Section presenting the planet
m^2
S
S
Section Tube
m^2
t
t
Time
s
V
V
Volume
m^3
J_V
J_V
Volume flow
m^3/s

Calculations


First, select the equation: to , then, select the variable: to
j_s = @DIFF( s , t , 1 ) J_V = @DIFF( V , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s V = s * S j_ssS_dStVJ_VV

Calculations

Symbol
Equation
Solved
Translated

Calculations

Symbol
Equation
Solved
Translated

Variable Given Calculate Target : Equation To be used
j_s = @DIFF( s , t , 1 ) J_V = @DIFF( V , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s V = s * S j_ssS_dStVJ_VV




Equations

#
Equation

j_s =\displaystyle\frac{ ds }{ dt }

j_s = @DIFF( s , t , 1 )


J_V =\displaystyle\frac{ dV }{ dt }

J_V = @DIFF( V , t , 1 )


J_V =\displaystyle\int j_s dS

J_V = @INT( j_s , S )


J_V = S j_s

J_V = S * j_s


V = s S

V = h * S

ID:(15714, 0)



Instant Volume Flow

Equation

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The volume flow (J_V) corresponds to the quantity volume (V) that flows through the channel during a time (t). Therefore, we have:

J_V =\displaystyle\frac{ dV }{ dt }

t
Time
s
10148
V
Volume
m^3
9847
J_V
Volume flow
m^3/s
5448
V = s * S J_V = @DIFF( V , t , 1 ) j_s = @DIFF( s , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s j_ssS_dStVJ_VV

The definition of the volume flow (J_V) is the volume element (\Delta V) over the time elapsed (\Delta t):

J_V =\displaystyle\frac{ \Delta V }{ \Delta t }



which, in the limit of an infinitesimal time interval, corresponds to the derivative of the volume (V) with respect to the time (t):

J_V =\displaystyle\frac{ dV }{ dt }

ID:(12713, 0)



Element volume

Equation

>Top, >Model


The volume (V) is calculated by multiplying the section Tube (S) with the position (s) along the tube:

V = s S

V = h S

h
s
Position
m
9849
S
Section presenting the planet
m^2
6700
V
Volumen
m^3
6699
V = s * S J_V = @DIFF( V , t , 1 ) j_s = @DIFF( s , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s j_ssS_dStVJ_VV

ID:(4876, 0)



Instantaneous flux density

Equation

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The flux density (j_s) is related to the position (s), which is the fluid position at the time (t), through the following equation:

j_s =\displaystyle\frac{ ds }{ dt }

j_s
Flux density
m/s
7220
s
Position
m
9849
t
Time
s
10148
V = s * S J_V = @DIFF( V , t , 1 ) j_s = @DIFF( s , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s j_ssS_dStVJ_VV

ID:(12714, 0)



Volume Flow and its Speed

Equation

>Top, >Model


A flux density (j_s) can be expressed in terms of the volume flow (J_V) using the section or Area (S) through the following formula:

J_V = S j_s

j_s
Flux density
m/s
7220
S
Section Tube
m^2
6267
J_V
Volume flow
m^3/s
5448
V = s * S J_V = @DIFF( V , t , 1 ) j_s = @DIFF( s , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s j_ssS_dStVJ_VV

The volume (V) for a tube with constant the section Tube (S) and a position (s) is

V = s S



If the section Tube (S) is constant, the temporal derivative will be

\displaystyle\frac{dV}{dt} = S\displaystyle\frac{ds}{dt}



thus, with the volume flow (J_V) defined by

J_V =\displaystyle\frac{ dV }{ dt }



and with the flux density (j_s) associated with the position (s) via

j_s =\displaystyle\frac{ ds }{ dt }



it is concluded that

J_V = S j_s

ID:(15716, 0)



Flow for inhomogeneous flux density

Equation

>Top, >Model


If the flux density (j_s) is not constant and varies across the flow tube section the volume flow (J_V), it is calculated as the integral over that section:

J_V =\displaystyle\int j_s dS

j_s
Flux density
m/s
7220
J_V
Volume flow
m^3/s
5448
V = s * S J_V = @DIFF( V , t , 1 ) j_s = @DIFF( s , t , 1 ) J_V = @INT( j_s , S ) J_V = S * j_s j_ssS_dStVJ_VV

In the case that the flux density (j_s) is constant, the volume flow (J_V) can be calculated using the section or Area (S) according to:

J_V = S j_s



If the flux density (j_s) varies, sufficiently small sectional elements dS can be considered so that the equation remains valid in the sense that the contribution to flow is:

dJ_V = j_s dS



Integrating this expression over the entire section results in

J_V =\displaystyle\int j_s dS

ID:(15712, 0)