Lift in an accelerated flight Calculator

Category	Physics ↺
Physics	Flight Stability and Control ↺
Flight-Stability-And-Control	Airplane Performance ↺
Airplane-Performance	Equations of Motion ↺

✖Mass is the quantity of matter in a body regardless of its volume or of any forces acting on it.ⓘ Mass [m]			+10% -10%
✖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]			+10% -10%
✖Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). ⓘ Velocity [v]			+10% -10%
✖In differential geometry, the radius of curvature, R, is the reciprocal of the curvature.ⓘ Radius of Curvature [r]			+10% -10%
✖Thrust force acting perpendicular to job pieceⓘ Thrust force [Ft]			+10% -10%
✖Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.ⓘ Thrust angle [α_T]			+10% -10%

✖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ⓘ Lift in an accelerated flight [L]

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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

Angular Displacement

Angular Displacement=Distance Covered on the Circular Path/Radius of Curvature GO

Air Resistance Force

Air Resistance=Air Constant*Velocity^2 GO

Specific Heat Capacity

Specific Heat Capacity=Energy Required/(Mass*Rise in Temperature) GO

Archimedes Principle

Archimedes Principle=Density*Acceleration Due To Gravity*Velocity GO

Tangential Acceleration

Tangential Acceleration=Angular Acceleration*Radius of Curvature GO

Potential Energy

Potential Energy=Mass*Acceleration Due To Gravity*Height GO

Angular Velocity

Angular velocity=Tangential Velocity/Radius of Curvature 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

Forces acting Perpendicular to the body on the flight path

Lift force=Weight*cos(Angle of Inclination)-Mass*((Velocity^2)/Radius) GO

Lift acting on aircraft during ground roll

Lift force=Weight-(Rolling Resistance/Coefficient of Rolling Friction) GO

Lift force for a body moving in a fluid of certain density

Lift force=lift coefficient*Reference Area*Density*(Velocity^2)/2 GO

Lift for an unaccelerated flight

Lift force=Weight-(Thrust of an aircraft*sin(Thrust angle)) GO

Lift for a level, unaccelerated flight at negligible thrust angle

Lift force=Dynamic Pressure*Area*lift coefficient GO

Lift Force

Lift force=lift coefficient*Dynamic Pressure*Area GO

Total Lift of wing-tail combination

Lift force=Lift due to wing+Lift due to tail GO

Lift force with angle of attack

Lift force=Drag Force*cot(Angle of attack) GO

Lift for given glide angle

Lift force=Drag Force/tan(Glide angle) GO

Lift during level turn

Lift force=Weight/cos(Bank angle) GO

Lift for a given load factor

Lift force=Load factor*Weight GO

Lift in an accelerated flight Formula

Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle))
L=(m*[g]*cos(θ))+(m*(v^2)/r)-(Ft*sin(α<sub>T</sub>))

More formulas

Thrust in an accelerated flight GO

Drag 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 happens to the lift if thrust increase?

If the thrust of an aircraft is increased, the aircraft will accelerate and the velocity will increase.

How to Calculate Lift in an accelerated flight?

Lift in an accelerated flight calculator uses Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle)) to calculate the Lift force, The Lift in an accelerated flight is a function of the weight of aircraft, flight velocity, the thrust of aircraft, thrust angle, flight path angle, and radius of curvature of the curved path. Lift force and is denoted by L symbol.

How to calculate Lift in an accelerated flight using this online calculator? To use this online calculator for Lift in an accelerated flight, enter Mass (m), Flight path angle (θ), Velocity (v), Radius of Curvature (r), Thrust force (Ft) and Thrust angle (α_T) and hit the calculate button. Here is how the Lift in an accelerated flight calculation can be explained with given input values -> 8855.083 = (35.45*[g]*cos(2.00535228295826))+(35.45*(60^2)/15)-(10*sin(2.00535228295826)).

FAQ

What is Lift in an accelerated flight?

The Lift in an accelerated flight is a function of the weight of aircraft, flight velocity, the thrust of aircraft, thrust angle, flight path angle, and radius of curvature of the curved path and is represented as L=(m*[g]*cos(θ))+(m*(v^2)/r)-(Ft*sin(α_T)) or Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle)). 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, Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). , In differential geometry, the radius of curvature, R, is the reciprocal of the curvature, Thrust force acting perpendicular to job piece and Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.

How to calculate Lift in an accelerated flight?

The Lift in an accelerated flight is a function of the weight of aircraft, flight velocity, the thrust of aircraft, thrust angle, flight path angle, and radius of curvature of the curved path is calculated using Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle)). To calculate Lift in an accelerated flight, you need Mass (m), Flight path angle (θ), Velocity (v), Radius of Curvature (r), Thrust force (Ft) and Thrust angle (α_T). With our tool, you need to enter the respective value for Mass, Flight path angle, Velocity, Radius of Curvature, Thrust force and Thrust angle 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 Lift force?

In this formula, Lift force uses Mass, Flight path angle, Velocity, Radius of Curvature, Thrust force and Thrust angle. We can use 11 other way(s) to calculate the same, which is/are as follows -

Lift force=lift coefficient*Dynamic Pressure*Area
Lift force=Weight*cos(Angle of Inclination)-Mass*((Velocity^2)/Radius)
Lift force=Weight-(Thrust of an aircraft*sin(Thrust angle))
Lift force=Dynamic Pressure*Area*lift coefficient
Lift force=Drag Force*cot(Angle of attack)
Lift force=Drag Force/tan(Glide angle)
Lift force=Weight-(Rolling Resistance/Coefficient of Rolling Friction)
Lift force=Weight/cos(Bank angle)
Lift force=Load factor*Weight
Lift force=Lift due to wing+Lift due to tail
Lift force=lift coefficient*Reference Area*Density*(Velocity^2)/2

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