Ishan Gupta
Birla Institute of Technology & Science (BITS), Pilani
Ishan Gupta has created this Calculator and 50+ more calculators!

4 Other formulas that you can solve using the same Inputs

Heat Exchanger Effectiveness
Effectiveness of Heat Exchanger= if(Mass of hot fluid*Specific Heat Capacity of Hot Fluid>Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid) { Effectiveness of Heat Exchanger=Mass of hot fluid*Specific Heat Capacity of Hot Fluid*(Inlet Temperature of Hot Fluid-Outlet Temperature of Hot Fluid)/(Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Hot Fluid-Inlet Temperature of Cold Fluid)) } else { Effectiveness of Heat Exchanger=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid)/(Mass of hot fluid*Specific Heat Capacity of Hot Fluid*(Inlet Temperature of Hot Fluid-Inlet Temperature of Cold Fluid)) } GO
Number of Transfer Units in a Heat Exchanger
Number of Transfer Units= if(Mass of hot fluid*Specific Heat Capacity of Hot Fluid>Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid) { Number of Transfer Units=Overall Heat Transfer Coefficient/(Area*Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid) } else { Number of Transfer Units=Overall Heat Transfer Coefficient/(Area*Mass of hot fluid*Specific Heat Capacity of Hot Fluid) } GO
Log Mean Temperature Difference for Counter Current Flow
Log Mean Temperature Difference=((Outlet Temperature of Hot Fluid-Inlet Temperature of Cold Fluid)-(Inlet Temperature of Hot Fluid-Outlet Temperature of Cold Fluid))/ln((Outlet Temperature of Hot Fluid-Inlet Temperature of Cold Fluid)/(Inlet Temperature of Hot Fluid-Outlet Temperature of Cold Fluid)) GO
Log Mean Temperature Difference for CoCurrent Flow
Log Mean Temperature Difference=((Outlet Temperature of Hot Fluid-Outlet Temperature of Cold Fluid)-(Inlet Temperature of Hot Fluid-Inlet Temperature of Cold Fluid))/ln((Outlet Temperature of Hot Fluid-Outlet Temperature of Cold Fluid)/(Inlet Temperature of Hot Fluid-Inlet Temperature of Cold Fluid)) GO

8 Other formulas that calculate the same Output

Radial Heat flowing through a cylinder
Heat=(Thermal Conductivity*2*pi*(outer radius-inner radius)*Temperature Difference*length of cylinder)/((ln(outer radius/inner radius))*(outer radius-inner radius)) GO
Heat Transfer in a Heat Exchanger using hot fluid properties
Heat=Mass of hot fluid*Specific Heat Capacity of Hot Fluid*(Inlet Temperature of Hot Fluid-Outlet Temperature of Hot Fluid) GO
Radiative Heat Transfer
Heat=[Stefan-BoltZ]*Body Surface Area*Geometric View Factor*(Temperature of surface 1^4-Temperature of surface 2^4) GO
Heat Transfer in an Isobaric Process
Heat=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference GO
Heat Transfer in an Isochoric Process
Heat=Number of Moles*Molar Specific Heat Capacity at Constant Volume*Temperature Difference GO
Heat Transfer in a Heat Exchanger using overall heat transfer coefficient
Heat=Overall Heat Transfer Coefficient*Area*(Outside Temperature-Inside Temperature) GO
Heat transferred in isothermal process (using pressure)
Heat=[R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System) GO
Heat transferred in isothermal process (using volume)
Heat=[R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System) GO

Heat Transfer in a Heat Exchanger using cold fluid properties Formula

Heat=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid)
More formulas
Heat Transfer Through Plane Wall or Surface GO
Critical Radius of Insulation of a Sphere GO
Critical Radius of Insulation of a Cylinder GO
Emmisive power of a body (Radiation) GO
Number of Transfer Units in a Heat Exchanger GO
Log Mean Temperature Difference for CoCurrent Flow GO
Log Mean Temperature Difference for Counter Current Flow GO
Heat Exchanger Effectiveness GO
Heat Transfer in a Heat Exchanger using overall heat transfer coefficient GO
Heat Transfer in a Heat Exchanger using hot fluid properties GO
Reynolds Number for Circular Tubes GO
Reynolds Number for Non-Circular Tubes GO
Prandtl Number GO
Nusselt Number for Transitional and Rough Flow in Circular Tube GO
Stanton Number (using dimensionless numbers) GO
Stanton Number (using basic fluid properties) GO
Thermal Diffusivity GO
Momentum Diffusivity GO
Prandtl Number (using diffusivities) GO
Radial Heat flowing through a cylinder GO
Radiative Heat Transfer GO

Heat Transfer in a Heat Exchanger

Heat Transfer in a Heat Exchanger gives the heat transferred from hot fluid to cold fluid.

How to Calculate Heat Transfer in a Heat Exchanger using cold fluid properties ?

Heat Transfer in a Heat Exchanger using cold fluid properties calculator uses Heat=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid) to calculate the Heat, Heat Transfer in a Heat Exchanger using cold fluid properties gives the heat energy transferred from the hot fluid to the cold fluid. Heat and is denoted by Q symbol.

How to calculate Heat Transfer in a Heat Exchanger using cold fluid properties using this online calculator? To use this online calculator for Heat Transfer in a Heat Exchanger using cold fluid properties , enter Specific Heat Capacity of Cold Fluid (cc), Mass of Cold Fluid (mc), Inlet Temperature of Cold Fluid (Tci) and Outlet Temperature of Cold Fluid (Tco) and hit the calculate button. Here is how the Heat Transfer in a Heat Exchanger using cold fluid properties calculation can be explained with given input values -> -500 = 10*10*(5-10).

FAQ

What is Heat Transfer in a Heat Exchanger using cold fluid properties ?
Heat Transfer in a Heat Exchanger using cold fluid properties gives the heat energy transferred from the hot fluid to the cold fluid and is represented as Q=mc*cc*(Tci-Tco) or Heat=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid). Specific Heat Capacity of Cold Fluid is a physical property of matter, defined as the amount of heat to be supplied to a unit mass of the cooler fluid to produce a unit change in its temperature, Mass of Cold Fluid is the mass of the cooler fluid in the heat exchanger, Inlet Temperature of Cold Fluid is the temperature at which the cold fluid enters the heat exchanger and Outlet Temperature of Cold Fluid is the temperature at which the cold fluid exits the heat exchanger.
How to calculate Heat Transfer in a Heat Exchanger using cold fluid properties ?
Heat Transfer in a Heat Exchanger using cold fluid properties gives the heat energy transferred from the hot fluid to the cold fluid is calculated using Heat=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid). To calculate Heat Transfer in a Heat Exchanger using cold fluid properties , you need Specific Heat Capacity of Cold Fluid (cc), Mass of Cold Fluid (mc), Inlet Temperature of Cold Fluid (Tci) and Outlet Temperature of Cold Fluid (Tco). With our tool, you need to enter the respective value for Specific Heat Capacity of Cold Fluid, Mass of Cold Fluid, Inlet Temperature of Cold Fluid and Outlet Temperature of Cold Fluid and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Heat?
In this formula, Heat uses Specific Heat Capacity of Cold Fluid, Mass of Cold Fluid, Inlet Temperature of Cold Fluid and Outlet Temperature of Cold Fluid. We can use 8 other way(s) to calculate the same, which is/are as follows -
  • Heat=Overall Heat Transfer Coefficient*Area*(Outside Temperature-Inside Temperature)
  • Heat=Mass of hot fluid*Specific Heat Capacity of Hot Fluid*(Inlet Temperature of Hot Fluid-Outlet Temperature of Hot Fluid)
  • Heat=Number of Moles*Molar Specific Heat Capacity at Constant Volume*Temperature Difference
  • Heat=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference
  • Heat=[R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System)
  • Heat=[R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System)
  • Heat=(Thermal Conductivity*2*pi*(outer radius-inner radius)*Temperature Difference*length of cylinder)/((ln(outer radius/inner radius))*(outer radius-inner radius))
  • Heat=[Stefan-BoltZ]*Body Surface Area*Geometric View Factor*(Temperature of surface 1^4-Temperature of surface 2^4)
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