Track of main Undercarriage given Radius of Fillet Solution

STEP 0: Pre-Calculation Summary
Formula Used
Track of Main Undercarriage = -2*(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+Minimum Safety Margin)
T = -2*(r-R+γ+M)
This formula uses 5 Variables
Variables Used
Track of Main Undercarriage - Track of Main Undercarriage considered. Undercarriage is a wheeled structure beneath an aircraft, typically retracted when not in use, which supports the aircraft on the ground.
Radius of Fillet - (Measured in Meter) - Radius of Fillet measured, a fillet is a rounding of an interior or exterior corner of a part design.
Radius of Taxiway Centerline - (Measured in Meter) - Radius of Taxiway Centerline taken as guideline, Taxiway centerlines are marked to provide a visual identification of the designated taxiing path.
Deviation of Main Undercarriage - Deviation of Main Undercarriage observed. The undercarriage of an airplane is the part, including the wheels, which supports the airplane when it is on the ground and when it is landing or taking off.
Minimum Safety Margin - Minimum Safety Margin, The margin of safety allows extra load range in the event the material is weaker than expected or an allowable load that may be higher than anticipated.
STEP 1: Convert Input(s) to Base Unit
Radius of Fillet: 27.5 Meter --> 27.5 Meter No Conversion Required
Radius of Taxiway Centerline: 150 Meter --> 150 Meter No Conversion Required
Deviation of Main Undercarriage: 95 --> No Conversion Required
Minimum Safety Margin: 15 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
T = -2*(r-R+γ+M) --> -2*(27.5-150+95+15)
Evaluating ... ...
T = 25
STEP 3: Convert Result to Output's Unit
25 --> No Conversion Required
FINAL ANSWER
25 <-- Track of Main Undercarriage
(Calculation completed in 00.004 seconds)

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Coorg Institute of Technology (CIT), Coorg
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12 Design of Fillets Calculators

Maximum value of Deviation of main Undercarriage given Radius of Fillet
Go Deviation of Main Undercarriage = -(Radius of Fillet-Radius of Taxiway Centerline+Minimum Safety Margin+(Track of Main Undercarriage/2))
Track of main Undercarriage given Radius of Fillet
Go Track of Main Undercarriage = -2*(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+Minimum Safety Margin)
Minimum Safety Margin given Radius of Fillet
Go Minimum Safety Margin = -(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+(Track of Main Undercarriage/2))
Radius of Fillet
Go Radius of Fillet = Radius of Taxiway Centerline-(Deviation of Main Undercarriage+Minimum Safety Margin+(Track of Main Undercarriage/2))
Radius of Taxiway Centerline given Radius of Fillet
Go Radius of Taxiway Centerline = Radius of Fillet+(Deviation of Main Undercarriage+Minimum Safety Margin+Track of Main Undercarriage/2)
Track of Main Undercarriage given Maximum Deviation permissible without Filleting
Go Track of Main Undercarriage = 2*((Taxiway Width/2)-Maximum Deviation without Filleting-Minimum Safety Margin)
Minimum Safety Margin given Maximum Deviation permissible without Filleting
Go Minimum Safety Margin = (Taxiway Width/2)-Maximum Deviation without Filleting-(Track of Main Undercarriage/2)
Taxiway Width given Maximum Deviation permissible without Filleting
Go Taxiway Width = 2*(Maximum Deviation without Filleting+(Minimum Safety Margin+Track of Main Undercarriage/2))
Maximum Deviation permissible without Filleting
Go Maximum Deviation without Filleting = (Taxiway Width/2)-(Minimum Safety Margin+Track of Main Undercarriage/2)
Distance along Straight Taxiway Center line given Length of each End of Fillet
Go Distance along Straight Taxiway Centerline = Length of each Wedge-shaped end of Fillet+Datum Length of Aircraft
Aircraft Datum Length given Length of each Wedge-shaped End of Fillet
Go Datum Length of Aircraft = Distance along Straight Taxiway Centerline-Length of each Wedge-shaped end of Fillet
Length of each Wedge-Shaped end of Fillet
Go Length of each Wedge-shaped end of Fillet = Distance along Straight Taxiway Centerline-Datum Length of Aircraft

Track of main Undercarriage given Radius of Fillet Formula

Track of Main Undercarriage = -2*(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+Minimum Safety Margin)
T = -2*(r-R+γ+M)

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 Track of main Undercarriage given Radius of Fillet?

Track of main Undercarriage given Radius of Fillet calculator uses Track of Main Undercarriage = -2*(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+Minimum Safety Margin) to calculate the Track of Main Undercarriage, Track of main Undercarriage given Radius of Fillet is defined as part, including wheels, which supports airplane when it is on ground and when it is landing or taking off. Track of Main Undercarriage is denoted by T symbol.

How to calculate Track of main Undercarriage given Radius of Fillet using this online calculator? To use this online calculator for Track of main Undercarriage given Radius of Fillet, enter Radius of Fillet (r), Radius of Taxiway Centerline (R), Deviation of Main Undercarriage (γ) & Minimum Safety Margin (M) and hit the calculate button. Here is how the Track of main Undercarriage given Radius of Fillet calculation can be explained with given input values -> 25 = -2*(27.5-150+95+15) .

FAQ

What is Track of main Undercarriage given Radius of Fillet?
Track of main Undercarriage given Radius of Fillet is defined as part, including wheels, which supports airplane when it is on ground and when it is landing or taking off and is represented as T = -2*(r-R+γ+M) or Track of Main Undercarriage = -2*(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+Minimum Safety Margin). Radius of Fillet measured, a fillet is a rounding of an interior or exterior corner of a part design, Radius of Taxiway Centerline taken as guideline, Taxiway centerlines are marked to provide a visual identification of the designated taxiing path, Deviation of Main Undercarriage observed. The undercarriage of an airplane is the part, including the wheels, which supports the airplane when it is on the ground and when it is landing or taking off & Minimum Safety Margin, The margin of safety allows extra load range in the event the material is weaker than expected or an allowable load that may be higher than anticipated.
How to calculate Track of main Undercarriage given Radius of Fillet?
Track of main Undercarriage given Radius of Fillet is defined as part, including wheels, which supports airplane when it is on ground and when it is landing or taking off is calculated using Track of Main Undercarriage = -2*(Radius of Fillet-Radius of Taxiway Centerline+Deviation of Main Undercarriage+Minimum Safety Margin). To calculate Track of main Undercarriage given Radius of Fillet, you need Radius of Fillet (r), Radius of Taxiway Centerline (R), Deviation of Main Undercarriage (γ) & Minimum Safety Margin (M). With our tool, you need to enter the respective value for Radius of Fillet, Radius of Taxiway Centerline, Deviation of Main Undercarriage & Minimum Safety Margin 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 Track of Main Undercarriage?
In this formula, Track of Main Undercarriage uses Radius of Fillet, Radius of Taxiway Centerline, Deviation of Main Undercarriage & Minimum Safety Margin. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Track of Main Undercarriage = 2*((Taxiway Width/2)-Maximum Deviation without Filleting-Minimum Safety Margin)
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