Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 200+ more calculators!
Sai Venkata Phanindra Chary Arendra
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Velocity in an accelerated flight
Velocity=((Radius of Curvature/Mass)*(Lift force+(Thrust force*sin(Thrust angle))-(Mass*[g]*cos(Flight path angle))))^(1/2) GO
Centrifugal Force in an accelerated flight
Centrifugal force=Lift force+(Thrust force*sin(Thrust angle))-(Mass*[g]*cos(Flight path angle)) GO
Coefficient of lift equation with angle of attack
lift coefficient=2*((sin(Angle of attack))^2)*cos(Angle of attack) GO
Thrust angle for an unaccelerated flight for given lift
Thrust angle=asin((Weight-Lift force)/Thrust of an aircraft) GO
Weight of aircraft in level, unaccelerated flight
Weight=Lift force+(Thrust of an aircraft*sin(Thrust angle)) GO
Coefficient of lift equation with coefficient of normal force
lift coefficient=coefficient of force*cos(Angle of attack) GO
Coefficient of drag equation with coefficient of normal force
Drag Coefficient=coefficient of force*sin(Angle of attack) GO
Dynamic pressure based on coefficient of lift
Dynamic Pressure=Lift force/(lift coefficient*Area) GO
lift coefficient
lift coefficient=Lift force/(Dynamic Pressure*Area) GO
Coefficient of drag equation with angle of attack
Drag Coefficient=2*(sin(Angle of attack))^3 GO
Lift force with angle of attack
Lift force=Drag Force*cot(Angle of attack) GO

11 Other formulas that calculate the same Output

Drag during ground effect
Drag Force=(Parasite Drag coefficient+(((lift coefficient^2)*Ground effect factor)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)))*(0.5*Freestream density*(Velocity^2)*Reference Area) GO
Drag in an accelerated flight
Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) GO
Drag force on the plate in boundary layer flow
Drag Force=0.73*Width*viscosity of fluid*Fluid Velocity*sqrt(Reynolds Number) GO
Drag force in falling sphere resistance method
Drag Force=3*pi*viscosity of fluid*velocity of sphere*diameter of sphere GO
Forces acting on body along the flight path
Drag Force=(Weight*sin(Angle of Inclination))-(Mass*Velocity Gradient) GO
Drag for a level, unaccelerated flight
Drag Force=Thrust of an aircraft*(cos(Thrust angle)) GO
Drag for a level, unaccelerated flight at negligible thrust angle
Drag Force=Dynamic Pressure*Area*Drag Coefficient GO
Drag force
Drag Force=Drag Coefficient*Dynamic Pressure*Area GO
Total Drag for given excess power
Drag Force=Thrust force-(Excess Power/Velocity) GO
Drag for given glide angle
Drag Force=Lift force*tan(Glide angle) GO
Total drag for given required power
Drag Force=Power/Freestream Velocity GO

Drag force with angle of attack Formula

Drag Force=Lift force/cot(Angle of attack)
F<sub>D</sub>=L/cot(α)
More formulas
Mass flux incident on a surface area GO
Time rate of change of momentum of the mass flux GO
Force F exerted on the surface GO
Coefficient of lift equation with coefficient of normal force GO
Coefficient of drag equation with coefficient of normal force GO
Coefficient of lift equation with angle of attack GO
Coefficient of drag equation with angle of attack GO
Lift force with angle of attack GO
Modified Newtonian Law GO
Maximum Pressure coefficient GO
exact normal shock-wave maximum coefficient of pressure GO
Pressure coefficient for slender 2-D bodies GO
Pressure coefficient for slender bodies of revolution GO

What is drag force?

A drag force is the resistance force caused by the motion of a body through a fluid, such as water or air. A drag force acts opposite to the direction of the oncoming flow velocity. This is the relative velocity between the body and the fluid.

How to Calculate Drag force with angle of attack?

Drag force with angle of attack calculator uses Drag Force=Lift force/cot(Angle of attack) to calculate the Drag Force, The Drag force with angle of attack formula is defined as the ratio of lift force to the cot of angle of attack. Drag Force and is denoted by FD symbol.

How to calculate Drag force with angle of attack using this online calculator? To use this online calculator for Drag force with angle of attack, enter Lift force (L) and Angle of attack (α) and hit the calculate button. Here is how the Drag force with angle of attack calculation can be explained with given input values -> 1.76327 = 10/cot(10).

FAQ

What is Drag force with angle of attack?
The Drag force with angle of attack formula is defined as the ratio of lift force to the cot of angle of attack and is represented as FD or Drag Force=Lift force/cot(Angle of attack). 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 and 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 Drag force with angle of attack?
The Drag force with angle of attack formula is defined as the ratio of lift force to the cot of angle of attack is calculated using Drag Force=Lift force/cot(Angle of attack). To calculate Drag force with angle of attack, you need Lift force (L) and Angle of attack (α). With our tool, you need to enter the respective value for Lift force and Angle of attack and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Drag Force?
In this formula, Drag Force uses Lift force and Angle of attack. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Drag Force=Drag Coefficient*Dynamic Pressure*Area
  • Drag Force=(Weight*sin(Angle of Inclination))-(Mass*Velocity Gradient)
  • Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration)
  • Drag Force=Thrust of an aircraft*(cos(Thrust angle))
  • Drag Force=Dynamic Pressure*Area*Drag Coefficient
  • Drag Force=Power/Freestream Velocity
  • Drag Force=Thrust force-(Excess Power/Velocity)
  • Drag Force=Lift force*tan(Glide angle)
  • Drag Force=(Parasite Drag coefficient+(((lift coefficient^2)*Ground effect factor)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)))*(0.5*Freestream density*(Velocity^2)*Reference Area)
  • Drag Force=3*pi*viscosity of fluid*velocity of sphere*diameter of sphere
  • Drag Force=0.73*Width*viscosity of fluid*Fluid Velocity*sqrt(Reynolds Number)
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