Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object Calculator

✖Separation Distance between Taxiway and respective masses located in space by a definite distance.ⓘ Separation Distance [S]			+10% -10%
✖Lateral Deviation is an asymmetry of the face when viewed from the front.ⓘ Lateral Deviation [d_L]			+10% -10%
✖Wing Tip Clearance that accounts for aircraft steering performance.ⓘ Wing Tip Clearance [Z]			+10% -10%

✖Span of wing given separation distance between aircraft stand taxi lane-to-object is the distance from one wingtip to the other wingtip.ⓘ Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object [W_Span]

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Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object Solution

STEP 0: Pre-Calculation Summary

Formula Used

Span of Wing = 2*(Separation Distance-Lateral Deviation-Wing Tip Clearance)
W_Span = 2*(S-d_L-Z)
This formula uses 4 Variables

Variables Used

Span of Wing - (Measured in Meter) - Span of wing given separation distance between aircraft stand taxi lane-to-object is the distance from one wingtip to the other wingtip.
Separation Distance - (Measured in Meter) - Separation Distance between Taxiway and respective masses located in space by a definite distance.
Lateral Deviation - Lateral Deviation is an asymmetry of the face when viewed from the front.
Wing Tip Clearance - (Measured in Meter) - Wing Tip Clearance that accounts for aircraft steering performance.

STEP 1: Convert Input(s) to Base Unit

Separation Distance: 64 Meter --> 64 Meter No Conversion Required
Lateral Deviation: 17.5 --> No Conversion Required
Wing Tip Clearance: 5 Meter --> 5 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

W_Span = 2*(S-d_L-Z) --> 2*(64-17.5-5)

Evaluating ... ...

W_Span = 83

STEP 3: Convert Result to Output's Unit

83 Meter --> No Conversion Required

FINAL ANSWER

83 Meter <-- Span of Wing

(Calculation completed in 00.004 seconds)

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Coorg Institute of Technology (CIT), Coorg

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Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object Formula

LaTeX Go

Span of Wing = 2*(Separation Distance-Lateral Deviation-Wing Tip Clearance)
W_Span = 2*(S-d_L-Z)

What is the function of Taxiway?

The functions of the Taxiway are to: Provide for aircraft to travel to and from runways to other areas of the airport in an expeditious manner. The system of taxiway is a decisive influence on the capacity of the runway system, and thereby also the overall capacity of the aerodrome.

How to Calculate Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object?

Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object calculator uses Span of Wing = 2*(Separation Distance-Lateral Deviation-Wing Tip Clearance) to calculate the Span of Wing, Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object is Given is defined as total stretch of airplane wings. Span of Wing is denoted by W_Span symbol.

How to calculate Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object using this online calculator? To use this online calculator for Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object, enter Separation Distance (S), Lateral Deviation (d_L) & Wing Tip Clearance (Z) and hit the calculate button. Here is how the Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object calculation can be explained with given input values -> 83 = 2*(64-17.5-5).

FAQ

What is Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object?

Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object is Given is defined as total stretch of airplane wings and is represented as W_Span = 2*(S-d_L-Z) or Span of Wing = 2*(Separation Distance-Lateral Deviation-Wing Tip Clearance). Separation Distance between Taxiway and respective masses located in space by a definite distance, Lateral Deviation is an asymmetry of the face when viewed from the front & Wing Tip Clearance that accounts for aircraft steering performance.

How to calculate Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object?

Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object is Given is defined as total stretch of airplane wings is calculated using Span of Wing = 2*(Separation Distance-Lateral Deviation-Wing Tip Clearance). To calculate Wing Span given Separation Distance between Aircraft Stand Taxi lane-to-object, you need Separation Distance (S), Lateral Deviation (d_L) & Wing Tip Clearance (Z). With our tool, you need to enter the respective value for Separation Distance, Lateral Deviation & Wing Tip Clearance 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 Span of Wing?

In this formula, Span of Wing uses Separation Distance, Lateral Deviation & Wing Tip Clearance. We can use 1 other way(s) to calculate the same, which is/are as follows -

Span of Wing = (Separation Distance-Clearance Distance-Wing Tip Clearance)/0.5

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