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 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(αT)) 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 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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