Anirudh Singh
National Institute of Technology (NIT), Jamshedpur
Anirudh Singh has created this Calculator and 100+ more calculators!

## < 11 Other formulas that you can solve using the same Inputs

Final Temperature in Adiabatic Process (using pressure)
final temp.=initial temp.*(Final Pressure of System/Initial Pressure of System)^(1-1/(Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume)) GO
Final Temperature in Adiabatic Process (using volume)
final temp.=initial temp.*(Final Volume of System/Initial Volume of System)^(1-Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume) GO
Entropy change (Isobaric Process) (With given temperatures)
Entropy change constant pressure=Mass of Gas*Molar Specific Heat Capacity at Constant Pressure*ln(final temp./initial temp.) GO
Entropy change (Isochoric Process) (With given temperatures)
Entropy change constant volume=Mass of Gas*Molar Specific Heat Capacity at Constant Volume*ln(final temp./initial temp.) GO
Temperature ratio at the start and end of ramming process
Temperature Ratio=1+(((Velocity^2)*(Heat Capacity Ratio-1)))/(2*(Heat Capacity Ratio*[R]*initial temp.)) GO
Heat Transfer at Constant Pressure
Heat Transfer=Mass of Gas*Molar Specific Heat Capacity at Constant Pressure*(final temp.-initial temp.) GO
Isobaric Work (for given mass and temperatures)
Isobaric work=Amount of Gaseous Substance in Moles*Universal Gas Constant*(final temp.-initial temp.) GO
Work =(Mass of Gas*[R]*(initial temp.-final temp.))/(Heat Capacity Ratio-1) GO
Temperature After a Given Time
Temperature=s temp.+(s temp.-initial temp.)*e^(-temp. constant*Time) GO
Carnot Cycle of Heat Engine
carnot cycle =1-(initial temp./final temp.) GO
Otto Cycle Efficiency
OTE=1-(initial temp./final temp.) GO

### By Pass Factor Formula

by pass factor=(intermediate temperature-final temp.)/ (intermediate temperature-initial temp.)
More formulas
Temperature After a Given Time GO
Mean Effective Pressure GO
Otto Cycle Efficiency GO
Degree of Saturation GO
Dew Point Depression GO
Carnot Cycle of Heat Engine GO
Absolute Humidity GO
Volumetric Efficiency GO
Partial pressure of Water Vapour GO
Diesel Efficiency GO
Indicated Thermal Efficiency GO
Brake Thermal Efficiency GO
Ranking Cycle Efficiency GO
Brayton Cycle Efficiency GO
Real Heat Pump GO
Real Heat Engine GO
Thermal Efficiency of Heat Engine GO
performance of heat pump GO
work of heat pump GO
Carnot Cycle of Heat Pump GO
Overall Efficiency GO
Sensible Heat Factor GO
Coefficient of Performance of absorption system GO
Refrigerator Work GO
Coefficient of Performance of Refrigerator GO
Carnot Cycle of Refrigerator GO
Real Refrigerator GO
Absolute Temperature GO
Turbine Efficiency GO
Compressor Efficiency GO
Cooled Compressor Efficiency GO
Nozzle Efficiency GO
Work done in an isobaric process GO
Relative Density GO
Density Of Two Liquids GO
Entropy Balance Equation GO
Specific Entropy GO
Air Fuel Ratio GO
Compressibility Factor GO
Reduced Temperature GO
Reduced Pressure GO
Pseudo-Reduced Specific volume GO
Degree Of Freedom GO
Helmholtz free energy GO
RMS speed GO
Average speed of gases GO
Most probable speed GO
Equipartition energy GO
Equipartition energy for molecule having n degrees of freedom GO
Molar internal energy of an ideal gas GO
Thermal efficiency given Mechanical energy GO
Thermal efficiency given Waste energy GO
Thermal efficiency of a Carnot engine GO
Coefficient of Performance of Refrigerator given the heat in the cold and hot reservoir GO
Coefficient of Performance of Heat Pump given the heat in the cold and hot reservoir GO
Coefficient of Performance of Heat Pump given work and heat in the cold reservoir GO
Coefficient of Performance of Refrigerator given work and heat in the cold reservoir GO
Change in momentum GO
Change in kinetic energy GO
Change in potential energy GO
Stefan–Boltzmann law GO
Newton's law of cooling GO
Pressure GO
Specific heat GO
Ratio of specific heat GO
Entropy change at constant volume GO
Entropy change at constant pressure GO
Entropy change variable specific heat GO
Specific heat ratio GO
Specific Heat of Gas Mixture GO
Molar Internal Energy of an Ideal Gas GO
Work Done in Isobaric Process GO
Ideal Gas Law for Calculating Volume GO
Ideal Gas Law for Calculating Pressure GO
Specific Gas Constant GO
Pressure Ratio in Isentropic Process GO
Temperature Ratio When Isentropic Pressure is Given GO
Temperature Ratio when Isentropic Specific Volume is Given GO
Isentropic Pressure at point 2 GO
Isentropic Pressure at point 1 GO
Isentropic temperature 2 given pressure ratio GO
Isentropic temperature 1 given pressure ratio GO
Isentropic temperature 1 given specific volume GO
Isentropic temperature 2 given specific volume GO
Relative Humidity GO
Specific Humidity GO
Vapour Quality GO
Saturated Mixture Specific Enthalpy GO
Isobaric work GO
Polytropic work GO
Isothermal work given volume ratio GO
Isothermal work given pressure ratio GO
Isothermal work given temperature GO
Shaft power GO
Spring work GO
Van der Waals equation GO
Irreversibility GO
Isothermal Work Done by the gas GO
Latent heat GO
Specific heat at constant volume GO
Isothermal Compression Of An Ideal Gas GO
Thermal stress of a material GO
Thermal Expansion GO
Internal Energy When Helmholtz Free Energy Is Given GO
Temperature When Helmholtz free Energy is Given GO
Entropy When Helmholtz Free Energy is Given GO
Temperature Of The Gas When RMS Velocity Of The Gas Is Given GO
Molar Mass Of The Gas When RMS Velocity Of The Gas Is Given GO
Temperature Of The Gas When Average Speed Of Gas Is Given GO
Molar Mass of the Gas When Average Speed of the Gas is Given GO
Temperature of the Gas When Most Probable Speed of Gas is Given GO
Molar Mass of the Gas When Most Probable Speed of the Gas is Given GO
Temperature of the Gas When Equipartition energy is Given GO
Temperature Of The Gas When Equipartition energy for molecule is Given GO
Degree of Freedom When Equipartition Energy is Given GO
Temperature of Ideal Gas When Internal Energy of the Ideal Gas is Given GO
Number of Moles When Internal Energy of Ideal Gas is Given GO
Degree of Freedom When Molar Internal Energy Of An Ideal Gas is Given GO

## What is By Pass Factor?

The inability of a coil to cool or heat the air to its temperature is indicated by a factor called by-pass factor (BPF) or Coil Bypass Factor. BPF can also be defined as the ratio of air which is unaffected by the coil to the total quantity of air passing over the coil.

## How to Calculate By Pass Factor?

By Pass Factor calculator uses by pass factor=(intermediate temperature-final temp.)/ (intermediate temperature-initial temp.) to calculate the by pass factor, By Pass Factor is the inability of a coil to cool or heat the air to its temperature. by pass factor and is denoted by BPF symbol.

How to calculate By Pass Factor using this online calculator? To use this online calculator for By Pass Factor, enter initial temp. (T0), final temp. (Tf) and intermediate temperature (Tint) and hit the calculate button. Here is how the By Pass Factor calculation can be explained with given input values -> 1 = (50-100)/ (50-100).

### FAQ

What is By Pass Factor?
By Pass Factor is the inability of a coil to cool or heat the air to its temperature and is represented as BPF=(Tint-Tf)/ (Tint-T0) or by pass factor=(intermediate temperature-final temp.)/ (intermediate temperature-initial temp.). initial temp. is temperature at start of the task, final temp. of a body is the temperature after complete process and intermediate temperature is temperature of a body at a certain intermediate state.
How to calculate By Pass Factor?
By Pass Factor is the inability of a coil to cool or heat the air to its temperature is calculated using by pass factor=(intermediate temperature-final temp.)/ (intermediate temperature-initial temp.). To calculate By Pass Factor, you need initial temp. (T0), final temp. (Tf) and intermediate temperature (Tint). With our tool, you need to enter the respective value for initial temp, final temp and intermediate temperature 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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