Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid Solution

STEP 0: Pre-Calculation Summary
Formula Used
Velocity of Flow at Nozzle Outlet = sqrt((2*Specific Heat Ratio*Pressure at Nozzle Inlet)/((Specific Heat Ratio+1)*Density of Air Medium))
Vf2 = sqrt((2*y*P1)/((y+1)*ρa))
This formula uses 1 Functions, 4 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
Velocity of Flow at Nozzle Outlet - (Measured in Meter per Second) - The Velocity of Flow at Nozzle Outlet is velocity of the fluid at the outlet of the orifice or the nozzle.
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 for non-viscous and compressible flow.
Pressure at Nozzle Inlet - (Measured in Pascal) - Pressure at Nozzle Inlet is the pressure of the fluid at the inlet point of the orifice or the nozzle.
Density of Air Medium - (Measured in Kilogram per Cubic Meter) - Density of Air Medium shows the denseness of the air. This is taken as mass per unit volume.
STEP 1: Convert Input(s) to Base Unit
Specific Heat Ratio: 1.4 --> No Conversion Required
Pressure at Nozzle Inlet: 70000 Newton per Square Meter --> 70000 Pascal (Check conversion here)
Density of Air Medium: 1.29 Kilogram per Cubic Meter --> 1.29 Kilogram per Cubic Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Vf2 = sqrt((2*y*P1)/((y+1)*ρa)) --> sqrt((2*1.4*70000)/((1.4+1)*1.29))
Evaluating ... ...
Vf2 = 251.609804141356
STEP 3: Convert Result to Output's Unit
251.609804141356 Meter per Second --> No Conversion Required
FINAL ANSWER
251.609804141356 251.6098 Meter per Second <-- Velocity of Flow at Nozzle Outlet
(Calculation completed in 00.004 seconds)

Credits

Created by Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has created this Calculator and 300+ more calculators!
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Calculator and 300+ more calculators!

10+ Compressible Flow Parameters Calculators

Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid
Go Velocity of Flow at Nozzle Outlet = sqrt((2*Specific Heat Ratio*Pressure at Nozzle Inlet)/((Specific Heat Ratio+1)*Density of Air Medium))
Pressure Ratio for Maximum Flow Rate through Nozzle
Go Pressure Ratio for Flow through Nozzle = (2/(Specific Heat Ratio+1))^(Specific Heat Ratio/(Specific Heat Ratio-1))
Velocity of Projectile of Mach Cone in Compressible Fluid Flow
Go Projectile Velocity of Mach Cone = Velocity of Sound in Medium/(sin(Mach Angle in Compressible Flow))
Mach Angle for Compressible Fluid Flow
Go Mach Angle in Compressible Flow = asin(Velocity of Sound in Medium/Projectile Velocity of Mach Cone)
Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow
Go Velocity of Sound in Medium = Projectile Velocity of Mach Cone*sin(Mach Angle in Compressible Flow)
Velocity of Sound Wave given Bulk Modulus
Go Velocity of Sound in Medium = sqrt(Bulk Modulus of Sound Medium/Density of Air Medium)
Sonic Velocity
Go Velocity of Sound in Medium = sqrt(Bulk Modulus of Sound Medium/Density of Air Medium)
Velocity of Sound Wave given Mach Number for Compressible Fluid Flow
Go Velocity of Sound in Medium = Projectile Velocity of Mach Cone/Mach Number for Compressible Flow
Mach Number for Compressible Fluid Flow
Go Mach Number for Compressible Flow = Projectile Velocity of Mach Cone/Velocity of Sound in Medium
Bulk Modulus for Velocity of Sound Wave
Go Bulk Modulus of Sound Medium = Density of Air Medium*Velocity of Sound in Medium^2

Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid Formula

Velocity of Flow at Nozzle Outlet = sqrt((2*Specific Heat Ratio*Pressure at Nozzle Inlet)/((Specific Heat Ratio+1)*Density of Air Medium))
Vf2 = sqrt((2*y*P1)/((y+1)*ρa))

What is mass flow rate in a compressible flow?

For a compressible, ideal gas, the mass flow rate is a unique function of the flow area, total pressure, the temperature of the flow, properties of the gas, and the Mach number.

How mass flow rate is related to pressure?

Bernoulli's equation states mathematically that if a fluid is flowing through a tube and the tube diameter decreases, then the velocity of the fluid increases, the pressure decreases, and the mass flow (and therefore volumetric flow) remains constant so long as the air density is constant.

How to Calculate Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid?

Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid calculator uses Velocity of Flow at Nozzle Outlet = sqrt((2*Specific Heat Ratio*Pressure at Nozzle Inlet)/((Specific Heat Ratio+1)*Density of Air Medium)) to calculate the Velocity of Flow at Nozzle Outlet, The Velocity at outlet of nozzle for maximum flow rate of fluid formula is known while considering the specific heat ratio, pressure at the inlet, and the density of fluid at point one. Velocity of Flow at Nozzle Outlet is denoted by Vf2 symbol.

How to calculate Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid using this online calculator? To use this online calculator for Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid, enter Specific Heat Ratio (y), Pressure at Nozzle Inlet (P1) & Density of Air Medium a) and hit the calculate button. Here is how the Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid calculation can be explained with given input values -> 251.6098 = sqrt((2*1.4*70000)/((1.4+1)*1.29)).

FAQ

What is Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid?
The Velocity at outlet of nozzle for maximum flow rate of fluid formula is known while considering the specific heat ratio, pressure at the inlet, and the density of fluid at point one and is represented as Vf2 = sqrt((2*y*P1)/((y+1)*ρa)) or Velocity of Flow at Nozzle Outlet = sqrt((2*Specific Heat Ratio*Pressure at Nozzle Inlet)/((Specific Heat Ratio+1)*Density of Air Medium)). The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow, Pressure at Nozzle Inlet is the pressure of the fluid at the inlet point of the orifice or the nozzle & Density of Air Medium shows the denseness of the air. This is taken as mass per unit volume.
How to calculate Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid?
The Velocity at outlet of nozzle for maximum flow rate of fluid formula is known while considering the specific heat ratio, pressure at the inlet, and the density of fluid at point one is calculated using Velocity of Flow at Nozzle Outlet = sqrt((2*Specific Heat Ratio*Pressure at Nozzle Inlet)/((Specific Heat Ratio+1)*Density of Air Medium)). To calculate Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid, you need Specific Heat Ratio (y), Pressure at Nozzle Inlet (P1) & Density of Air Medium a). With our tool, you need to enter the respective value for Specific Heat Ratio, Pressure at Nozzle Inlet & Density of Air Medium and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!