Lift Force with Angle of Attack Solution

STEP 0: Pre-Calculation Summary
Formula Used
Lift Force = Drag Force*cot(Angle of Attack)
FL = FD*cot(α)
This formula uses 1 Functions, 3 Variables
Functions Used
cot - Cotangent is a trigonometric function that is defined as the ratio of the adjacent side to the opposite side in a right triangle., cot(Angle)
Variables Used
Lift Force - (Measured in Newton) - The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
Angle of Attack - (Measured in Radian) - Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.
STEP 1: Convert Input(s) to Base Unit
Drag Force: 80 Newton --> 80 Newton No Conversion Required
Angle of Attack: 10.94 Degree --> 0.190939020168144 Radian (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
FL = FD*cot(α) --> 80*cot(0.190939020168144)
Evaluating ... ...
FL = 413.877808485416
STEP 3: Convert Result to Output's Unit
413.877808485416 Newton --> No Conversion Required
FINAL ANSWER
413.877808485416 413.8778 Newton <-- Lift Force
(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna
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14 Newtonian Flow Calculators

Time Rate of Change of Momentum of Mass Flux
​ Go Force = Density of Fluid*Fluid Velocity^2*Area*(sin(Angle of Inclination))^2
Mass Flux Incident on Surface Area
​ Go Mass Flux(g) = Density of Material*Velocity*Area*sin(Angle of Inclination)
Maximum Pressure Coefficient
​ Go Maximum Pressure Coefficient = (Total Pressure-Pressure)/(0.5*Density of Material*Freestream Velocity^2)
Exact Normal Shock Wave Maximum Coefficient of Pressure
​ Go Maximum Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*(Total Pressure/Pressure-1)
Pressure Coefficient for Slender 2D Bodies
​ Go Pressure Coefficient = 2*((Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis)
Pressure Coefficient for Slender Bodies of Revolution
​ Go Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis
Coefficient of Lift Equation with Angle of Attack
​ Go Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(Angle of Attack)
Modified Newtonian Law
​ Go Pressure Coefficient = Maximum Pressure Coefficient*(sin(Angle of Inclination))^2
Coefficient of Lift Equation with Coefficient of Normal Force
​ Go Lift Coefficient = Coefficient of Force*cos(Angle of Attack)
Coefficient of Drag Equation with Coefficient of Normal Force
​ Go Drag Coefficient = Coefficient of Force*sin(Angle of Attack)
Force Exerted on Surface given Static Pressure
​ Go Force = Area*(Surface Pressure-Static Pressure)
Lift Force with Angle of Attack
​ Go Lift Force = Drag Force*cot(Angle of Attack)
Drag Force with Angle of Attack
​ Go Drag Force = Lift Force/cot(Angle of Attack)
Coefficient of Drag Equation with Angle of Attack
​ Go Drag Coefficient = 2*(sin(Angle of Attack))^3

Lift Force with Angle of Attack Formula

Lift Force = Drag Force*cot(Angle of Attack)
FL = FD*cot(α)

What is Lift force?

A fluid flowing around the surface of an object exerts a force on it. Lift is the component of this force that is perpendicular to the oncoming flow direction.

How to Calculate Lift Force with Angle of Attack?

Lift Force with Angle of Attack calculator uses Lift Force = Drag Force*cot(Angle of Attack) to calculate the Lift Force, The Lift force with angle of attack formula is defined as the product of drag force and cot of angle of attack. Lift Force is denoted by FL symbol.

How to calculate Lift Force with Angle of Attack using this online calculator? To use this online calculator for Lift Force with Angle of Attack, enter Drag Force (FD) & Angle of Attack (α) and hit the calculate button. Here is how the Lift Force with Angle of Attack calculation can be explained with given input values -> 413.8778 = 80*cot(0.190939020168144).

FAQ

What is Lift Force with Angle of Attack?
The Lift force with angle of attack formula is defined as the product of drag force and cot of angle of attack and is represented as FL = FD*cot(α) or Lift Force = Drag Force*cot(Angle of Attack). Drag Force is the resisting force experienced by an object moving through a fluid & Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.
How to calculate Lift Force with Angle of Attack?
The Lift force with angle of attack formula is defined as the product of drag force and cot of angle of attack is calculated using Lift Force = Drag Force*cot(Angle of Attack). To calculate Lift Force with Angle of Attack, you need Drag Force (FD) & Angle of Attack (α). With our tool, you need to enter the respective value for Drag Force & Angle of Attack 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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