Heat Absorbed during Constant pressure Expansion Process Calculator

Category	Engineering ↺
Engineering	Mechanical ↺
Mechanical	Refrigeration and Air Conditioning ↺
Refrigeration-And-Air-Conditioning	Air Refrigeration Cycles ↺
Air-Refrigeration-Cycles	Bell-Coleman Cycle or Reversed Brayton or Joule Cycle ↺

✖Specific heat capacity at constant pressure means the amount of heat that is required to raise the temperature of a unit mass of gas by 1 degree at constant pressure.ⓘ Specific Heat Capacity at Constant Pressure [C_p]			+10% -10%
✖The temperature at the start of Isentropic Compression is the temperature from which the cycle starts.ⓘ Temperature at the start of Isentropic Compression [T₁]			+10% -10%
✖Temperature at the end of Isentropic Expansion is the temperature from where isentropic expansion ends and isobaric expansion starts.ⓘ Temperature at the end of Isentropic Expansion [T₄]			+10% -10%

✖Heat Absorbed is the heat gained by any substance during any of the thermodynamic processes.ⓘ Heat Absorbed during Constant pressure Expansion Process [Q_Ad]

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Rushi Shah

K J Somaiya College of Engineering (K J Somaiya), Mumbai

Rushi Shah has created this Calculator and 3+ more calculators!

Mayank Tayal

National Institute of Technology (NIT), Durgapur

Mayank Tayal has verified this Calculator and 10+ more calculators!

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

Power required to maintain pressure inside the cabin(excluding ram work)

Input Power=((Mass of air*Specific Heat Capacity at Constant Pressure*Actual temperature of Rammed Air)/(Compressor efficiency))*((Cabin Pressure/Pressure of rammed air)^((Heat Capacity Ratio-1)/Heat Capacity Ratio)-1) GO

Power required to maintain pressure inside the cabin(including ram work)

Input Power=((Mass of air*Specific Heat Capacity at Constant Pressure*Ambient air temperature)/(Compressor efficiency))*((Cabin Pressure/Atmospheric Pressure)^((Heat Capacity Ratio-1)/Heat Capacity Ratio)-1) GO

C.O.P. of simple air evaporative cycle

Actual Coefficient of Performance=(210*Tonnage of Refrigeration)/(Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air)) GO

Mass of air to produce Q tonnes of refrigeration

Mass of air=(210*Tonnage of Refrigeration)/(1000*Specific Heat Capacity at Constant Pressure*(Temperature at the end of Isentropic Expansion-Actual exit Temperature of cooling turbine)) GO

Mass of air to produce Q tonnes of refrigeration

Mass of air=(210*Tonnage of Refrigeration)/(Specific Heat Capacity at Constant Pressure*(Inside temperature of cabin-Actual temperature at end of isentropic expansion)) GO

Refrigeration Effect Produced

Refrigeration Effect Produced=Mass of air*Specific Heat Capacity at Constant Pressure*(Inside temperature of cabin-Actual temperature at end of isentropic expansion) GO

Heat rejected during cooling process

Heat Rejected=Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Temperature at the end of cooling process) GO

Expansion Work

Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Temperature at the end of cooling process-Actual temperature at end of isentropic expansion) GO

Power required for refrigeration system

Input Power=(Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air))/60 GO

Heat Rejected during Constant pressure Cooling Process

Heat Rejected=Specific Heat Capacity at Constant Pressure*(Ideal temp at end of isentropic compression-Ideal temp at the end of isobaric cooling) GO

Compression Work

Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air) GO

Heat Absorbed during Constant pressure Expansion Process Formula

Heat Absorbed=Specific Heat Capacity at Constant Pressure*(Temperature at the start of Isentropic Compression-Temperature at the end of Isentropic Expansion)

More formulas

Heat Rejected during Constant pressure Cooling Process GO

Compression or Expansion Ratio GO

COP of Bell-Coleman Cycle for given Compression ratio and adiabatic index(γ) GO

What is heat Rejected during Constant pressure Cooling Process?

Heat Rejected during Constant pressure Cooling Process (q_A) is the heat absorbed by the air during constant pressure expansion process.

How to Calculate Heat Absorbed during Constant pressure Expansion Process?

Heat Absorbed during Constant pressure Expansion Process calculator uses Heat Absorbed=Specific Heat Capacity at Constant Pressure*(Temperature at the start of Isentropic Compression-Temperature at the end of Isentropic Expansion) to calculate the Heat Absorbed, Heat Absorbed during Constant pressure Expansion Process = Specific heat capacity constant pressure * (temperature at the start of Isentropic Compression - temperature at the end of Isentropic expansion). Heat Absorbed and is denoted by Q_Ad symbol.

How to calculate Heat Absorbed during Constant pressure Expansion Process using this online calculator? To use this online calculator for Heat Absorbed during Constant pressure Expansion Process, enter Temperature at the start of Isentropic Compression (T₁), Temperature at the end of Isentropic Expansion (T₄) and Specific Heat Capacity at Constant Pressure (C_p) and hit the calculate button. Here is how the Heat Absorbed during Constant pressure Expansion Process calculation can be explained with given input values -> 216 = 8*(300-273).

FAQ

What is Heat Absorbed during Constant pressure Expansion Process?

Heat Absorbed during Constant pressure Expansion Process = Specific heat capacity constant pressure * (temperature at the start of Isentropic Compression - temperature at the end of Isentropic expansion) and is represented as Q_Ad=C_p*(T₁-T₄) or Heat Absorbed=Specific Heat Capacity at Constant Pressure*(Temperature at the start of Isentropic Compression-Temperature at the end of Isentropic Expansion). The temperature at the start of Isentropic Compression is the temperature from which the cycle starts, Temperature at the end of Isentropic Expansion is the temperature from where isentropic expansion ends and isobaric expansion starts and Specific heat capacity at constant pressure means the amount of heat that is required to raise the temperature of a unit mass of gas by 1 degree at constant pressure.

How to calculate Heat Absorbed during Constant pressure Expansion Process?

Heat Absorbed during Constant pressure Expansion Process = Specific heat capacity constant pressure * (temperature at the start of Isentropic Compression - temperature at the end of Isentropic expansion) is calculated using Heat Absorbed=Specific Heat Capacity at Constant Pressure*(Temperature at the start of Isentropic Compression-Temperature at the end of Isentropic Expansion). To calculate Heat Absorbed during Constant pressure Expansion Process, you need Temperature at the start of Isentropic Compression (T₁), Temperature at the end of Isentropic Expansion (T₄) and Specific Heat Capacity at Constant Pressure (C_p). With our tool, you need to enter the respective value for Temperature at the start of Isentropic Compression, Temperature at the end of Isentropic Expansion and Specific Heat Capacity at Constant Pressure 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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