Maximum Blade Efficiency Solution

STEP 0: Pre-Calculation Summary
Formula Used
Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1)
nbm = (2*Fl/Fd-1)/(2*Fl/Fd+1)
This formula uses 3 Variables
Variables Used
Maximum Blade Efficiency - Maximum Blade Efficiency is the maximum efficiency with which the transfer of energy takes place to the moving blades.
Blade Lift Force - (Measured in Newton) - Blade Lift Force is the sum of all the forces acting on a blade that force it to move perpendicular to the direction of flow.
Blade Drag Force - (Measured in Newton) - Blade Drag Force is the resisting force experienced by the blades moving through a fluid.
STEP 1: Convert Input(s) to Base Unit
Blade Lift Force: 100 Newton --> 100 Newton No Conversion Required
Blade Drag Force: 19.7 Newton --> 19.7 Newton No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
nbm = (2*Fl/Fd-1)/(2*Fl/Fd+1) --> (2*100/19.7-1)/(2*100/19.7+1)
Evaluating ... ...
nbm = 0.820664542558034
STEP 3: Convert Result to Output's Unit
0.820664542558034 --> No Conversion Required
FINAL ANSWER
0.820664542558034 0.820665 <-- Maximum Blade Efficiency
(Calculation completed in 00.004 seconds)

Credits

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Created by Kaki Varun Krishna
Mahatma Gandhi Institute of Technology (MGIT), Hyderabad
Kaki Varun Krishna has created this Calculator and 25+ more calculators!
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Verified by Saurabh Patil
Shri Govindram Seksaria Institute of Technology and Science (SGSITS ), Indore
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9 Structural Design Calculators

Ultimate Tensile Stress for Plate
​ Go Ultimate Tensile Strength = (Edge Load per Unit Width*Distance between Rivets)/(Plate Thickness*(Distance between Rivets-Diameter of Rivet))
Shear Failure Load on plate
​ Go Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets)
Maximum Blade Efficiency
​ Go Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1)
Allowable Bearing Pressure
​ Go Bearing Stress = (Edge Load per Unit Width*Distance between Rivets)/(Plate Thickness*Diameter of Rivet)
Shear Load per width
​ Go Edge Load per Unit Width = (pi*(Diameter^2)*Maximum Shear Stress)/(4*Distance between Rivets)
Joint Efficiency
​ Go Joint Efficiency for Shell = (Distance between Rivets-Diameter)/(Distance between Rivets)
Disk Loading
​ Go Load = Aircraft Weight/((pi*Diameter of Rotor^2)/4)
Average Blade Lift Coefficient
​ Go Blade Lift Coefficient = 6*Thrust Coefficient/Rotor Solidity
Life of Aircraft given number of Flight
​ Go Number of Flights = (1/Total Damage per Flight)

Maximum Blade Efficiency Formula

Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1)
nbm = (2*Fl/Fd-1)/(2*Fl/Fd+1)

What is lift force and drag force?

A fluid flowing around an object exerts a force on it. Lift is the component of this force that is perpendicular to the oncoming flow direction. It contrasts with the drag force, which is the component of the force parallel to the flow direction.

How to Calculate Maximum Blade Efficiency?

Maximum Blade Efficiency calculator uses Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1) to calculate the Maximum Blade Efficiency, Maximum blade efficiency refers to the highest level of effectiveness with which a rotor blade converts the available energy in the airflow into useful mechanical energy, typically rotational motion, it represents the optimal performance state of the rotor blade, where it generates the maximum lift or thrust for a given input of power or energy. Maximum Blade Efficiency is denoted by nbm symbol.

How to calculate Maximum Blade Efficiency using this online calculator? To use this online calculator for Maximum Blade Efficiency, enter Blade Lift Force (Fl) & Blade Drag Force (Fd) and hit the calculate button. Here is how the Maximum Blade Efficiency calculation can be explained with given input values -> 0.820665 = (2*100/19.7-1)/(2*100/19.7+1).

FAQ

What is Maximum Blade Efficiency?
Maximum blade efficiency refers to the highest level of effectiveness with which a rotor blade converts the available energy in the airflow into useful mechanical energy, typically rotational motion, it represents the optimal performance state of the rotor blade, where it generates the maximum lift or thrust for a given input of power or energy and is represented as nbm = (2*Fl/Fd-1)/(2*Fl/Fd+1) or Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1). Blade Lift Force is the sum of all the forces acting on a blade that force it to move perpendicular to the direction of flow & Blade Drag Force is the resisting force experienced by the blades moving through a fluid.
How to calculate Maximum Blade Efficiency?
Maximum blade efficiency refers to the highest level of effectiveness with which a rotor blade converts the available energy in the airflow into useful mechanical energy, typically rotational motion, it represents the optimal performance state of the rotor blade, where it generates the maximum lift or thrust for a given input of power or energy is calculated using Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1). To calculate Maximum Blade Efficiency, you need Blade Lift Force (Fl) & Blade Drag Force (Fd). With our tool, you need to enter the respective value for Blade Lift Force & Blade Drag Force 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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