Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle Calculator

✖Lifting Force of Aircraft provided by the wing-body of the vehicle. Lift is defined as the component of the aerodynamic force that is perpendicular to the flow direction.ⓘ Lifting Force of Aircraft [L_Aircraft]			+10% -10%
✖Density Altitude for flying is a representation of the amount of mass of a substance, material or object in relation to the space it occupies at an altitude.ⓘ Density Altitude for flying [ρ]			+10% -10%
✖Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing.ⓘ Aircraft Gross Wing Area [S]			+10% -10%
✖The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.ⓘ Lift Coefficient [C_l]			+10% -10%

✖Vehicle Speed (True Air Speed) of an aircraft is the speed of aircraft relative to air mass through which it is flying. The true airspeed is important information for accurate navigation of aircraft.ⓘ Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle [V]

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Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle Solution

STEP 0: Pre-Calculation Summary

Formula Used

Vehicle Speed = sqrt((Lifting Force of Aircraft/(0.5*Density Altitude for flying*Aircraft Gross Wing Area*Lift Coefficient)))
V = sqrt((L_Aircraft/(0.5*ρ*S*C_l)))
This formula uses 1 Functions, 5 Variables

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Vehicle Speed - (Measured in Kilometer per Hour) - Vehicle Speed (True Air Speed) of an aircraft is the speed of aircraft relative to air mass through which it is flying. The true airspeed is important information for accurate navigation of aircraft.
Lifting Force of Aircraft - (Measured in Kilonewton) - Lifting Force of Aircraft provided by the wing-body of the vehicle. Lift is defined as the component of the aerodynamic force that is perpendicular to the flow direction.
Density Altitude for flying - (Measured in Kilogram per Cubic Meter) - Density Altitude for flying is a representation of the amount of mass of a substance, material or object in relation to the space it occupies at an altitude.
Aircraft Gross Wing Area - (Measured in Square Meter) - Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing.
Lift Coefficient - The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

STEP 1: Convert Input(s) to Base Unit

Lifting Force of Aircraft: 1072.39 Kilonewton --> 1072.39 Kilonewton No Conversion Required
Density Altitude for flying: 1.21 Kilogram per Cubic Meter --> 1.21 Kilogram per Cubic Meter No Conversion Required
Aircraft Gross Wing Area: 23 Square Meter --> 23 Square Meter No Conversion Required
Lift Coefficient: 0.001 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V = sqrt((L_Aircraft/(0.5*ρ*S*C_l))) --> sqrt((1072.39/(0.5*1.21*23*0.001)))

Evaluating ... ...

V = 277.60978670769

STEP 3: Convert Result to Output's Unit

77.1138296410251 Meter per Second -->277.60978670769 Kilometer per Hour (Check conversion here)

FINAL ANSWER

277.60978670769 ≈ 277.6098 Kilometer per Hour <-- Vehicle Speed

(Calculation completed in 00.004 seconds)

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Created by Mithila Muthamma PA

Coorg Institute of Technology (CIT), Coorg

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National Institute of Technology (NIT), Warangal

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< Aircraft Runway Length Estimation Calculators

Operating Empty Weight when Desired Take-off Weight is considered

LaTeX Go Operating Empty Weight = Desired Takeoff Weight of Aircraft-Payload Carried-Fuel Weight to be carried

Payload carried when desired take-off weight is considered

LaTeX Go Payload Carried = Desired Takeoff Weight of Aircraft-Operating Empty Weight-Fuel Weight to be carried

Fuel Weight to be Carried given Desired Takeoff Weight

LaTeX Go Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight

Desired Take off Weight

LaTeX Go Desired Takeoff Weight of Aircraft = Payload Carried+Operating Empty Weight+Fuel Weight to be carried

Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle Formula

LaTeX Go

Vehicle Speed = sqrt((Lifting Force of Aircraft/(0.5*Density Altitude for flying*Aircraft Gross Wing Area*Lift Coefficient)))
V = sqrt((L_Aircraft/(0.5*ρ*S*C_l)))

What is lift as a force?

Lift is the force that directly opposes the weight of an airplane and holds the airplane in the air. Lift is a mechanical aerodynamic force produced by the motion of the airplane through the air. Because lift is a force, it is a vector quantity, having both a magnitude and a direction associated with it.

What does drag force mean?

Drag is the aerodynamic force that opposes an aircraft's motion through the air. Drag is generated by the difference in velocity between the solid object and the fluid. There must be motion between the object and the fluid. If there is no motion, there is no drag.

How to Calculate Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle?

Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle calculator uses Vehicle Speed = sqrt((Lifting Force of Aircraft/(0.5*Density Altitude for flying*Aircraft Gross Wing Area*Lift Coefficient))) to calculate the Vehicle Speed, Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle is defined as the rate at which the vehicle moves or travels. Vehicle Speed is denoted by V symbol.

How to calculate Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle using this online calculator? To use this online calculator for Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle, enter Lifting Force of Aircraft (L_Aircraft), Density Altitude for flying (ρ), Aircraft Gross Wing Area (S) & Lift Coefficient (C_l) and hit the calculate button. Here is how the Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle calculation can be explained with given input values -> 999.3952 = sqrt((1072390/(0.5*1.21*23*0.001))).

FAQ

What is Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle?

Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle is defined as the rate at which the vehicle moves or travels and is represented as V = sqrt((L_Aircraft/(0.5*ρ*S*C_l))) or Vehicle Speed = sqrt((Lifting Force of Aircraft/(0.5*Density Altitude for flying*Aircraft Gross Wing Area*Lift Coefficient))). Lifting Force of Aircraft provided by the wing-body of the vehicle. Lift is defined as the component of the aerodynamic force that is perpendicular to the flow direction, Density Altitude for flying is a representation of the amount of mass of a substance, material or object in relation to the space it occupies at an altitude, Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing & The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

How to calculate Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle?

Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle is defined as the rate at which the vehicle moves or travels is calculated using Vehicle Speed = sqrt((Lifting Force of Aircraft/(0.5*Density Altitude for flying*Aircraft Gross Wing Area*Lift Coefficient))). To calculate Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle, you need Lifting Force of Aircraft (L_Aircraft), Density Altitude for flying (ρ), Aircraft Gross Wing Area (S) & Lift Coefficient (C_l). With our tool, you need to enter the respective value for Lifting Force of Aircraft, Density Altitude for flying, Aircraft Gross Wing Area & Lift Coefficient 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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