Nusselt intpipe
Returns the Nusselt number for a fluid going through a pipe.
Controller: CodeCogs
| doubleNusselt_intpipe( | double | Pr | |
| double | Gr | ||
| double | Re | )[inline] |
This module calculates the Nusselt number for a fluid which flows through a pipe, the flow being either laminar or turbulent. The fluid must keep its state of matter during the heat transfer process.
The formulae for each case are given by
and
where
is the Reynolds number,
is the Prandtl number and
is the Grashof number of the fluid. If the Reynolds number is less than 2000 the flow is considered laminar, while if it is greater than 4000 the flow is considered turbulent.
In the diagrams below the unit heat flow is shown in the laminar and turbulent regimes.


Example 1
- The following code calculates the Nusselt number for Air at 65 degrees Celsius flowing throug a pipe at 25 degrees with diameter of 0.5 meters. Both the laminar and turbulent cases are considered.
#include <codecogs/engineering/heat_transfer/convection/nusselt_intpipe.h> #include <stdio.h> int main() { double Pr = 0.70849, Gr = 384057065.8607, Re1 = 800, Re2 = 5100; printf("\nAir at 65 deg. Celsius\n"); printf("flowing through a pipe at 25 deg. Celsius\n\n"); printf("Re = %.2lf (laminar flow)\n", Re1); printf("Nu = %.4lf\n\n", Engineering::Heat_Transfer::Convection::Nusselt_intpipe(Pr, Gr, Re1)); printf("Re = %.2lf (turbulent flow)\n", Re2); printf("Nu = %.4lf\n\n", Engineering::Heat_Transfer::Convection::Nusselt_intpipe(Pr, Gr, Re2)); return 0; }
Output
Air at 65 deg. Celsius flowing through a pipe at 25 deg. Celsius Re = 800.00 (laminar flow) Nu = 8.4761 Re = 5100.00 (turbulent flow) Nu = 16.7463
References
- Dan Stefanescu, Mircea Marinescu - "Termotehnica"
Parameters
Pr the Prandtl number of the fluid Gr the Grashof number of the fluid Re the Reynolds number of the fluid
Returns
- the Nusselt number of the fluid with given parameters
Authors
- Grigore Bentea, Lucian Bentea (November 2006)
Source Code
Source code is available when you buy a Commercial licence.
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