Weight of aircraft during ground roll Calculator

✖Rolling Resistance (or Rolling friction) is the force resisting the motion of a rolling body on a surface.ⓘ Rolling Resistance [R]			+10% -10%
✖Coefficient of Rolling Friction is the ratio of the force of rolling friction to the total weight of the object.ⓘ Coefficient of Rolling Friction [μ_r]			+10% -10%
✖The Lift, 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 [F_L]			+10% -10%

✖Weight Newton is a vector quantity and defined as the product of mass and acceleration acting on that mass.ⓘ Weight of aircraft during ground roll [W]

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Weight of aircraft during ground roll Solution

STEP 0: Pre-Calculation Summary

Formula Used

Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift
W = (R/μ_r)+F_L
This formula uses 4 Variables

Variables Used

Weight - (Measured in Newton) - Weight Newton is a vector quantity and defined as the product of mass and acceleration acting on that mass.
Rolling Resistance - (Measured in Newton) - Rolling Resistance (or Rolling friction) is the force resisting the motion of a rolling body on a surface.
Coefficient of Rolling Friction - Coefficient of Rolling Friction is the ratio of the force of rolling friction to the total weight of the object.
Lift - (Measured in Newton) - The Lift, 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.

STEP 1: Convert Input(s) to Base Unit

Rolling Resistance: 5 Newton --> 5 Newton No Conversion Required
Coefficient of Rolling Friction: 0.1 --> No Conversion Required
Lift: 10.5 Newton --> 10.5 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

W = (R/μ_r)+F_L --> (5/0.1)+10.5

Evaluating ... ...

W = 60.5

STEP 3: Convert Result to Output's Unit

60.5 Newton --> No Conversion Required

FINAL ANSWER

60.5 Newton <-- Weight

(Calculation completed in 00.020 seconds)

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Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Shikha Maurya

Indian Institute of Technology (IIT), Bombay

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Coefficient of rolling friction during ground roll

LaTeX Go Coefficient of Rolling Friction = Rolling Resistance/(Weight-Lift)

Lift acting on aircraft during ground roll

LaTeX Go Lift = Weight-(Rolling Resistance/Coefficient of Rolling Friction)

Weight of aircraft during ground roll

LaTeX Go Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift

Resistance force during ground roll

LaTeX Go Rolling Resistance = Coefficient of Rolling Friction*(Weight-Lift)

Weight of aircraft during ground roll Formula

LaTeX Go

Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift
W = (R/μ_r)+F_L

How do planes steer on the ground?

Steering on the ground is achieved by turning the nose wheel, either by a tiller wheel in the cockpit or by using the rudder pedals.

How to Calculate Weight of aircraft during ground roll?

Weight of aircraft during ground roll calculator uses Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift to calculate the Weight, Weight of Aircraft During Ground Roll is a measure of the total weight of an aircraft during the ground roll phase of takeoff, calculated by considering the rolling resistance, friction coefficient, and lift force, providing a crucial parameter for aircraft performance and safety analysis. Weight is denoted by W symbol.

How to calculate Weight of aircraft during ground roll using this online calculator? To use this online calculator for Weight of aircraft during ground roll, enter Rolling Resistance (R), Coefficient of Rolling Friction (μ_r) & Lift (F_L) and hit the calculate button. Here is how the Weight of aircraft during ground roll calculation can be explained with given input values -> 60.5 = (5/0.1)+10.5.

FAQ

What is Weight of aircraft during ground roll?

Weight of Aircraft During Ground Roll is a measure of the total weight of an aircraft during the ground roll phase of takeoff, calculated by considering the rolling resistance, friction coefficient, and lift force, providing a crucial parameter for aircraft performance and safety analysis and is represented as W = (R/μ_r)+F_L or Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift. Rolling Resistance (or Rolling friction) is the force resisting the motion of a rolling body on a surface, Coefficient of Rolling Friction is the ratio of the force of rolling friction to the total weight of the object & The Lift, 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.

How to calculate Weight of aircraft during ground roll?

Weight of Aircraft During Ground Roll is a measure of the total weight of an aircraft during the ground roll phase of takeoff, calculated by considering the rolling resistance, friction coefficient, and lift force, providing a crucial parameter for aircraft performance and safety analysis is calculated using Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift. To calculate Weight of aircraft during ground roll, you need Rolling Resistance (R), Coefficient of Rolling Friction (μ_r) & Lift (F_L). With our tool, you need to enter the respective value for Rolling Resistance, Coefficient of Rolling Friction & Lift 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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