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Angular Momentum in a turbomachine refers to the rotational motion imparted to the fluid as it passes through the blades of the machine. Check FAQs
L=ct1r1
L - Angular Momentum?ct1 - Tangential Velocity at Inlet?r1 - Inlet Radius?

Angular Moment of Momentum at Inlet Example

With values
With units
Only example

Here is how the Angular Moment of Momentum at Inlet equation looks like with Values.

Here is how the Angular Moment of Momentum at Inlet equation looks like with Units.

Here is how the Angular Moment of Momentum at Inlet equation looks like.

106.4Edit=13.3Edit8Edit
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Angular Moment of Momentum at Inlet Solution

Follow our step by step solution on how to calculate Angular Moment of Momentum at Inlet?

FIRST Step Consider the formula
L=ct1r1
Next Step Substitute values of Variables
L=13.3m/s8m
Next Step Prepare to Evaluate
L=13.38
LAST Step Evaluate
L=106.4kg*m²/s

Angular Moment of Momentum at Inlet Formula Elements

Variables
Angular Momentum
Angular Momentum in a turbomachine refers to the rotational motion imparted to the fluid as it passes through the blades of the machine.
Symbol: L
Measurement: Angular MomentumUnit: kg*m²/s
Note: Value can be positive or negative.
Tangential Velocity at Inlet
Tangential Velocity at Inlet is the velocity of fluid at inlet direction normal to any radius.
Symbol: ct1
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Inlet Radius
Inlet Radius is the radius at the entry of a turbomachine.
Symbol: r1
Measurement: LengthUnit: m
Note: Value should be greater than 0.

Other Formulas to find Angular Momentum

​Go Angular Moment of Momentum at Exit
L=ct2re

Other formulas in Turbomachinery Equations category

​Go Peripheral Velocity of Blade at Exit corresponding to Diameter
u2=πDeN60
​Go Peripheral Velocity of Blade at Entry corresponding to Diameter
u1=πDiN60
​Go Torque Produced
τ=ct2re-ct1r1
​Go Energy Transfer due to Change of Absolute Kinetic Energy of Fluid
E=c12-c222

How to Evaluate Angular Moment of Momentum at Inlet?

Angular Moment of Momentum at Inlet evaluator uses Angular Momentum = Tangential Velocity at Inlet*Inlet Radius to evaluate the Angular Momentum, The Angular moment of momentum at inlet formula is defined as the product of tangential velocity at inlet and radius. Angular Momentum is denoted by L symbol.

How to evaluate Angular Moment of Momentum at Inlet using this online evaluator? To use this online evaluator for Angular Moment of Momentum at Inlet, enter Tangential Velocity at Inlet (ct1) & Inlet Radius (r1) and hit the calculate button.

FAQs on Angular Moment of Momentum at Inlet

What is the formula to find Angular Moment of Momentum at Inlet?
The formula of Angular Moment of Momentum at Inlet is expressed as Angular Momentum = Tangential Velocity at Inlet*Inlet Radius. Here is an example- 106.4 = 13.3*8.
How to calculate Angular Moment of Momentum at Inlet?
With Tangential Velocity at Inlet (ct1) & Inlet Radius (r1) we can find Angular Moment of Momentum at Inlet using the formula - Angular Momentum = Tangential Velocity at Inlet*Inlet Radius.
What are the other ways to Calculate Angular Momentum?
Here are the different ways to Calculate Angular Momentum-
  • Angular Momentum=Tangential Velocity at Exit*Exit RadiusOpenImg
Can the Angular Moment of Momentum at Inlet be negative?
Yes, the Angular Moment of Momentum at Inlet, measured in Angular Momentum can be negative.
Which unit is used to measure Angular Moment of Momentum at Inlet?
Angular Moment of Momentum at Inlet is usually measured using the Kilogram Square Meter per Second[kg*m²/s] for Angular Momentum. are the few other units in which Angular Moment of Momentum at Inlet can be measured.
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