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Drag in an accelerated flight Calculator

Category Physics ↺
Physics Flight Stability and Control ↺
Flight-Stability-And-Control Airplane Performance ↺
Airplane-Performance Equations of Motion ↺
✖The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.ⓘ Thrust of an aircraft [T]
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✖Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.ⓘ Thrust angle [αT]
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✖Mass is the quantity of matter in a body regardless of its volume or of any forces acting on it.ⓘ Mass [m]
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✖Flight path angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descendingⓘ Flight path angle [θ]
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✖Acceleration is the rate of change in velocity to the change in time.ⓘ Acceleration [a]
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✖Drag Force is the resisting force experienced by an object moving through a fluidⓘ Drag in an accelerated flight [FD
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Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra 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

Displacement of Body when initial velocity, time and acceleration are given
Displacement of Body=(Initial Velocity*Time Taken to Travel)+(Acceleration*(Time Taken to Travel)^2)/2 GO
Displacement of Body when initial velocity, final velocity and acceleration are given
Displacement of Body=((Final Velocity)^2-(Initial Velocity)^2)/(2*Acceleration) GO
Final Velocity of body
Final Velocity=Initial Velocity+Acceleration*(Time Taken to Travel) GO
Specific Heat Capacity
Specific Heat Capacity=Energy Required/(Mass*Rise in Temperature) GO
Centripetal Force or Centrifugal Force when angular velocity, mass and radius of curvature are given
Centripetal Force=Mass*(Angular velocity^2)*Radius of Curvature GO
Distance Traveled
Distance Traveled=Initial Velocity*T+(1/2)*Acceleration*(T)^2 GO
Potential Energy
Potential Energy=Mass*Acceleration Due To Gravity*Height GO
Centripetal Force
Centripetal Force=(Mass*(Velocity)^2)/Radius GO
Kinetic Energy
Kinetic Energy=(Mass*Velocity^2)/2 GO
Force
Force=Mass*Acceleration GO
Density
Density=Mass/Volume 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 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 force with angle of attack
Drag Force=Lift force/cot(Angle of attack) 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 in an accelerated flight Formula

Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration)
F<sub>D</sub>=(T*cos(α<sub>T</sub>))-(m*[g]*(sin(θ)))-(m*a)
More formulas
Thrust in an accelerated flight GO
Lift in an accelerated flight GO
Centrifugal Force in an accelerated flight GO
Velocity in an accelerated flight GO
Thrust for a level, unaccelerated flight GO
Drag for a level, unaccelerated flight GO
Thrust angle for an unaccelerated flight for given drag GO
Lift for an unaccelerated flight GO
Weight of aircraft in level, unaccelerated flight GO
Thrust angle for an unaccelerated flight for given lift GO

What is drag in flight?

Drag is the force that resists the movement of an aircraft through the air. There are two basic types: parasite drag and induced drag.

How to Calculate Drag in an accelerated flight?

Drag in an accelerated flight calculator uses Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) to calculate the Drag Force, The Drag in an accelerated flight is a function of thrust, weight, thrust angle, flight path angle, and acceleration of aircraft. Drag Force and is denoted by FD symbol.

How to calculate Drag in an accelerated flight using this online calculator? To use this online calculator for Drag in an accelerated flight, enter Thrust of an aircraft (T), Thrust angle (αT), Mass (m), Flight path angle (θ) and Acceleration (a) and hit the calculate button. Here is how the Drag in an accelerated flight calculation can be explained with given input values -> -337.626361 = (100*cos(2.00535228295826))-(35.45*[g]*(sin(2.00535228295826)))-(35.45*12).

FAQ

What is Drag in an accelerated flight?
The Drag in an accelerated flight is a function of thrust, weight, thrust angle, flight path angle, and acceleration of aircraft and is represented as FDT))-(m*[g]*(sin(θ)))-(m*a) or Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration). The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air, Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction, Mass is the quantity of matter in a body regardless of its volume or of any forces acting on it, Flight path angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descending and Acceleration is the rate of change in velocity to the change in time.
How to calculate Drag in an accelerated flight?
The Drag in an accelerated flight is a function of thrust, weight, thrust angle, flight path angle, and acceleration of aircraft is calculated using Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration). To calculate Drag in an accelerated flight, you need Thrust of an aircraft (T), Thrust angle (αT), Mass (m), Flight path angle (θ) and Acceleration (a). With our tool, you need to enter the respective value for Thrust of an aircraft, Thrust angle, Mass, Flight path angle and Acceleration 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 Thrust of an aircraft, Thrust angle, Mass, Flight path angle and Acceleration. 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))
  • Drag Force=Dynamic Pressure*Area*Drag Coefficient
  • Drag Force=Lift force/cot(Angle of attack)
  • 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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