Choked Mass Flow Rate given specific heat ratio Solution

STEP 0: Pre-Calculation Summary
Formula Used
Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2)))
choke = (γ/(sqrt(γ-1)))*((γ+1)/2)^(-((γ+1)/(2*γ-2)))
This formula uses 1 Functions, 2 Variables
Functions Used
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)
Variables Used
Choked Mass Flow Rate - Choked Mass Flow Rate refers to the maximum mass flow rate of a compressible fluid through a restricted flow area, reaching the critical sonic conditions.
Heat Capacity Ratio - Heat Capacity Ratio is the ratio of the specific heat at constant pressure (Cp) to the specific heat at constant volume (Cv) for a given substance.
STEP 1: Convert Input(s) to Base Unit
Heat Capacity Ratio: 1.4 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
choke = (γ/(sqrt(γ-1)))*((γ+1)/2)^(-((γ+1)/(2*γ-2))) --> (1.4/(sqrt(1.4-1)))*((1.4+1)/2)^(-((1.4+1)/(2*1.4-2)))
Evaluating ... ...
choke = 1.28101525585525
STEP 3: Convert Result to Output's Unit
1.28101525585525 --> No Conversion Required
FINAL ANSWER
1.28101525585525 1.281015 <-- Choked Mass Flow Rate
(Calculation completed in 00.004 seconds)

Credits

Created by Shreyash
Rajiv Gandhi Institute of Technology (RGIT), Mumbai
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19 Thermodynamics and Governing Equations Calculators

Max work output in Brayton cycle
Go Maximum Work done in Brayton Cycle = (1005*1/Compressor Efficiency)*Temperature at Inlet of Compressor in Brayton*(sqrt(Temperature at Inlet to Turbine in Brayton Cycle/Temperature at Inlet of Compressor in Brayton*Compressor Efficiency*Turbine Efficiency)-1)^2
Choked Mass Flow Rate given specific heat ratio
Go Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2)))
Choked Mass Flow Rate
Go Choked Mass Flow Rate = (Mass Flow Rate*sqrt(Specific Heat Capacity at Constant Pressure*Temperature))/(Nozzle Throat Area*Throat Pressure)
Stagnation Velocity of Sound given Specific Heat at Constant Pressure
Go Stagnation Velocity of Sound = sqrt((Heat Capacity Ratio-1)*Specific Heat Capacity at Constant Pressure*Stagnation Temperature)
Specific Heat of mixed out gas
Go Specific Heat of Mixed Gas = (Specific Heat of Core Gas+Bypass Ratio*Specific Heat of Bypass Air)/(1+Bypass Ratio)
Stagnation Temperature
Go Stagnation Temperature = Static Temperature+(Flow Velocity Downstream of Sound^2)/(2*Specific Heat Capacity at Constant Pressure)
Stagnation Velocity of Sound
Go Stagnation Velocity of Sound = sqrt(Heat Capacity Ratio*[R]*Stagnation Temperature)
Speed of Sound
Go Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
Stagnation Velocity of Sound given Stagnation Enthalpy
Go Stagnation Velocity of Sound = sqrt((Heat Capacity Ratio-1)*Stagnation Enthalpy)
Heat Capacity Ratio
Go Heat Capacity Ratio = Specific Heat Capacity at Constant Pressure/Specific Heat Capacity at Constant Volume
Efficiency of cycle
Go Efficiency of Cycle = (Turbine Work-Compressor Work)/Heat
Internal Energy of Perfect Gas at given Temperature
Go Internal Energy = Specific Heat Capacity at Constant Volume*Temperature
Enthalpy of Ideal Gas at given Temperature
Go Enthalpy = Specific Heat Capacity at Constant Pressure*Temperature
Stagnation enthalpy
Go Stagnation Enthalpy = Enthalpy+(Velocity of Fluid Flow^2)/2
Efficiency of Joule cycle
Go Efficiency of Joule Cycle = Net Work Output/Heat
Pressure Ratio
Go Pressure Ratio = Final Pressure/Initial Pressure
Work ratio in practical cycle
Go Work Ratio = 1-(Compressor Work/Turbine Work)
Mach Number
Go Mach Number = Speed of Object/Speed of Sound
Mach Angle
Go Mach Angle = asin(1/Mach Number)

Choked Mass Flow Rate given specific heat ratio Formula

Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2)))
choke = (γ/(sqrt(γ-1)))*((γ+1)/2)^(-((γ+1)/(2*γ-2)))

What is mass flow rate?

The amount of mass that flows through an area in a given amount of time is known as the mass flow rate. It is a measurement of the velocity at which gases and liquids pass through a specified area. It is an important factor that determines the amount of thrust produced.

What is specific heat ratio?

The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid.

How to Calculate Choked Mass Flow Rate given specific heat ratio?

Choked Mass Flow Rate given specific heat ratio calculator uses Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2))) to calculate the Choked Mass Flow Rate, The Choked Mass Flow Rate given specific heat ratio formulas describes when the engine gets maximum mass flow rate through the nozzle. It is observed when the Mach number is equal to one. The limiting of the mass flow rate is called choking of the flow. Choked Mass Flow Rate is denoted by choke symbol.

How to calculate Choked Mass Flow Rate given specific heat ratio using this online calculator? To use this online calculator for Choked Mass Flow Rate given specific heat ratio, enter Heat Capacity Ratio (γ) and hit the calculate button. Here is how the Choked Mass Flow Rate given specific heat ratio calculation can be explained with given input values -> 1.281015 = (1.4/(sqrt(1.4-1)))*((1.4+1)/2)^(-((1.4+1)/(2*1.4-2))).

FAQ

What is Choked Mass Flow Rate given specific heat ratio?
The Choked Mass Flow Rate given specific heat ratio formulas describes when the engine gets maximum mass flow rate through the nozzle. It is observed when the Mach number is equal to one. The limiting of the mass flow rate is called choking of the flow and is represented as choke = (γ/(sqrt(γ-1)))*((γ+1)/2)^(-((γ+1)/(2*γ-2))) or Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2))). Heat Capacity Ratio is the ratio of the specific heat at constant pressure (Cp) to the specific heat at constant volume (Cv) for a given substance.
How to calculate Choked Mass Flow Rate given specific heat ratio?
The Choked Mass Flow Rate given specific heat ratio formulas describes when the engine gets maximum mass flow rate through the nozzle. It is observed when the Mach number is equal to one. The limiting of the mass flow rate is called choking of the flow is calculated using Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2))). To calculate Choked Mass Flow Rate given specific heat ratio, you need Heat Capacity Ratio (γ). With our tool, you need to enter the respective value for Heat Capacity Ratio 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 Choked Mass Flow Rate?
In this formula, Choked Mass Flow Rate uses Heat Capacity Ratio. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Choked Mass Flow Rate = (Mass Flow Rate*sqrt(Specific Heat Capacity at Constant Pressure*Temperature))/(Nozzle Throat Area*Throat Pressure)
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