Jet velocity given temperature drop Solution

STEP 0: Pre-Calculation Summary
Formula Used
Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Temperature Drop)
Cideal = sqrt(2*Cp*ΔT)
This formula uses 1 Functions, 3 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
Ideal Exit Velocity - (Measured in Meter per Second) - Ideal Exit Velocity is the velocity at the exit of nozzle, it does not includes losses due to external factors.
Specific Heat at Constant Pressure - (Measured in Joule per Kilogram per K) - Specific heat at constant pressure is the energy required to raise the temperature of the unit mass of a substance by one degree as the pressure is maintained constant.
Temperature Drop - (Measured in Kelvin) - Temperature Drop is the difference between two temperatures.
STEP 1: Convert Input(s) to Base Unit
Specific Heat at Constant Pressure: 1248 Joule per Kilogram per K --> 1248 Joule per Kilogram per K No Conversion Required
Temperature Drop: 16 Kelvin --> 16 Kelvin No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Cideal = sqrt(2*Cp*ΔT) --> sqrt(2*1248*16)
Evaluating ... ...
Cideal = 199.839935948749
STEP 3: Convert Result to Output's Unit
199.839935948749 Meter per Second --> No Conversion Required
FINAL ANSWER
199.839935948749 199.8399 Meter per Second <-- Ideal Exit Velocity
(Calculation completed in 00.004 seconds)

Credits

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Created by Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!
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Verified by Sagar S Kulkarni
Dayananda Sagar College of Engineering (DSCE), Bengaluru
Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

Nozzle Calculators

Kinetic Energy of Exhaust Gases
​ LaTeX ​ Go Kinetic Energy of Gas = 1/2*Ideal Mass Flow Rate*(1+Fuel to Air Ratio)*Ideal Exit Velocity^2
Jet velocity given temperature drop
​ LaTeX ​ Go Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Temperature Drop)
Ideal Exhaust Velocity given Enthalpy Drop
​ LaTeX ​ Go Ideal Exit Velocity = sqrt(2*Enthalpy Drop in Nozzle)
Velocity Coefficient given Nozzle Efficiency
​ LaTeX ​ Go Velocity Coefficient = sqrt(Nozzle Efficiency)

Jet velocity given temperature drop Formula

​LaTeX ​Go
Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Temperature Drop)
Cideal = sqrt(2*Cp*ΔT)

What is enthalpy?

Enthalpy is a property of a thermodynamic system, defined as the sum of the system's internal energy and the product of its pressure and volume.

How to Calculate Jet velocity given temperature drop?

Jet velocity given temperature drop calculator uses Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Temperature Drop) to calculate the Ideal Exit Velocity, The Jet velocity given temperature drop formula is defined as the square root of 2 times the product of specific heat at constant pressure and temperature drop. Ideal Exit Velocity is denoted by Cideal symbol.

How to calculate Jet velocity given temperature drop using this online calculator? To use this online calculator for Jet velocity given temperature drop, enter Specific Heat at Constant Pressure (Cp) & Temperature Drop (ΔT) and hit the calculate button. Here is how the Jet velocity given temperature drop calculation can be explained with given input values -> 193.4942 = sqrt(2*1248*16).

FAQ

What is Jet velocity given temperature drop?
The Jet velocity given temperature drop formula is defined as the square root of 2 times the product of specific heat at constant pressure and temperature drop and is represented as Cideal = sqrt(2*Cp*ΔT) or Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Temperature Drop). Specific heat at constant pressure is the energy required to raise the temperature of the unit mass of a substance by one degree as the pressure is maintained constant & Temperature Drop is the difference between two temperatures.
How to calculate Jet velocity given temperature drop?
The Jet velocity given temperature drop formula is defined as the square root of 2 times the product of specific heat at constant pressure and temperature drop is calculated using Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Temperature Drop). To calculate Jet velocity given temperature drop, you need Specific Heat at Constant Pressure (Cp) & Temperature Drop (ΔT). With our tool, you need to enter the respective value for Specific Heat at Constant Pressure & Temperature Drop 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 Ideal Exit Velocity?
In this formula, Ideal Exit Velocity uses Specific Heat at Constant Pressure & Temperature Drop. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Ideal Exit Velocity = sqrt(2*Enthalpy Drop in Nozzle)
  • Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Nozzle Temperature*(1-(Pressure Ratio)^((Specific Heat Ratio-1)/(Specific Heat Ratio))))
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