Peripheral Velocity of Blade at Exit corresponding to Diameter Solution

STEP 0: Pre-Calculation Summary
Formula Used
Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60
u2 = (pi*De*N)/60
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Peripheral Velocity at Exit - (Measured in Meter per Second) - Peripheral Velocity at Exit is the speed that a point in the circumference moves per second.
Blade Diameter at Exit - (Measured in Meter) - Blade Diameter at Exit refers to the diameter of the blades or rotor at the exit section of a turbomachinery system.
Speed in RPM - Speed in RPM is the number of turns of the object divided by time, specified as revolutions per minute (rpm).
STEP 1: Convert Input(s) to Base Unit
Blade Diameter at Exit: 0.7 Meter --> 0.7 Meter No Conversion Required
Speed in RPM: 500 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
u2 = (pi*De*N)/60 --> (pi*0.7*500)/60
Evaluating ... ...
u2 = 18.3259571459405
STEP 3: Convert Result to Output's Unit
18.3259571459405 Meter per Second --> No Conversion Required
FINAL ANSWER
18.3259571459405 18.32596 Meter per Second <-- Peripheral Velocity at Exit
(Calculation completed in 00.004 seconds)

Credits

Created by Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
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8 Turbomachinery Equations Calculators

Torque Produced
Go Torque = Tangential Velocity at Exit*Exit Radius-Tangential Velocity at Inlet*Inlet Radius
Peripheral Velocity of Blade at Entry corresponding to Diameter
Go Peripheral Velocity at Inlet = (pi*Blade Diameter at Inlet*Speed in RPM)/60
Peripheral Velocity of Blade at Exit corresponding to Diameter
Go Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60
Energy Transfer due to Centrifugal Effect
Go Energy Transfer = (Peripheral Velocity at Inlet^2-Peripheral Velocity at Exit^2)/2
Energy Transfer due to Change of Absolute Kinetic Energy of Fluid
Go Energy Transfer = (Absolute Velocity at Inlet^2-Absolute Velocity at Exit^2)/2
Energy Transfer due to Change of Relative Kinetic Energy of Fluid
Go Energy Transfer = (Relative Velocity at Exit^2-Relative Velocity at Inlet^2)/2
Angular Moment of Momentum at Inlet
Go Angular Momentum = Tangential Velocity at Inlet*Inlet Radius
Angular Moment of Momentum at Exit
Go Angular Momentum = Tangential Velocity at Exit*Exit Radius

Peripheral Velocity of Blade at Exit corresponding to Diameter Formula

Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60
u2 = (pi*De*N)/60

What is Peripheral velocity?

Peripheral velocity is defined as the speed that a point in the circumference moves per second. It has both magnitude and direction.

How to Calculate Peripheral Velocity of Blade at Exit corresponding to Diameter?

Peripheral Velocity of Blade at Exit corresponding to Diameter calculator uses Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60 to calculate the Peripheral Velocity at Exit, The Peripheral Velocity of Blade at Exit corresponding to Diameter formula is defined as the π times the product of the speed of rotor and diameter, divided by 60. Peripheral Velocity at Exit is denoted by u2 symbol.

How to calculate Peripheral Velocity of Blade at Exit corresponding to Diameter using this online calculator? To use this online calculator for Peripheral Velocity of Blade at Exit corresponding to Diameter, enter Blade Diameter at Exit (De) & Speed in RPM (N) and hit the calculate button. Here is how the Peripheral Velocity of Blade at Exit corresponding to Diameter calculation can be explained with given input values -> 261.7994 = (pi*0.7*500)/60.

FAQ

What is Peripheral Velocity of Blade at Exit corresponding to Diameter?
The Peripheral Velocity of Blade at Exit corresponding to Diameter formula is defined as the π times the product of the speed of rotor and diameter, divided by 60 and is represented as u2 = (pi*De*N)/60 or Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60. Blade Diameter at Exit refers to the diameter of the blades or rotor at the exit section of a turbomachinery system & Speed in RPM is the number of turns of the object divided by time, specified as revolutions per minute (rpm).
How to calculate Peripheral Velocity of Blade at Exit corresponding to Diameter?
The Peripheral Velocity of Blade at Exit corresponding to Diameter formula is defined as the π times the product of the speed of rotor and diameter, divided by 60 is calculated using Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60. To calculate Peripheral Velocity of Blade at Exit corresponding to Diameter, you need Blade Diameter at Exit (De) & Speed in RPM (N). With our tool, you need to enter the respective value for Blade Diameter at Exit & Speed in RPM 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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