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Aircraft Mechanics
Blade Lift Coefficient in Conceptual Design Formulas
Blade Lift Coefficient is the lift coefficient of blades and is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body. And is denoted by C
l
.
Formulas to find Blade Lift Coefficient in Conceptual Design
f
x
Average Blade Lift Coefficient
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List of variables in Conceptual Design formulas
f
x
Thrust Coefficient
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f
x
Rotor Solidity
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FAQ
What is the Blade Lift Coefficient?
Blade Lift Coefficient is the lift coefficient of blades and is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body.
Can the Blade Lift Coefficient be negative?
{YesorNo}, the Blade Lift Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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