Maximum value of Deviation of main Undercarriage given Radius of Fillet Calculator

✖Radius of Fillet measured, a fillet is a rounding of an interior or exterior corner of a part design.ⓘ Radius of Fillet [r]			+10% -10%
✖Radius of Taxiway Centerline taken as guideline, Taxiway centerlines are marked to provide a visual identification of the designated taxiing path.ⓘ Radius of Taxiway Centerline [R]			+10% -10%
✖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.ⓘ Minimum Safety Margin [M]			+10% -10%
✖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.ⓘ Track of Main Undercarriage [T]			+10% -10%

✖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.ⓘ Maximum value of Deviation of main Undercarriage given Radius of Fillet [γ]

⎘ Copy

👎

Formula

✖

Maximum value of Deviation of main Undercarriage given Radius of Fillet

Formula

`"γ" = -("r"-"R"+"M"+("T"/2))`

Example

`"104"=-("27.5m"-"150m"+"15"+("7"/2))`

Calculator

LaTeX

Reset

👍

Download Taxiway Design Formulas PDF

Maximum value of Deviation of main Undercarriage given Radius of Fillet Solution

STEP 0: Pre-Calculation Summary

Formula Used

Deviation of Main Undercarriage = -(Radius of Fillet-Radius of Taxiway Centerline+Minimum Safety Margin+(Track of Main Undercarriage/2))
γ = -(r-R+M+(T/2))
This formula uses 5 Variables

Variables Used

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.
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.
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.
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.

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
Minimum Safety Margin: 15 --> No Conversion Required
Track of Main Undercarriage: 7 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

γ = -(r-R+M+(T/2)) --> -(27.5-150+15+(7/2))

Evaluating ... ...

γ = 104

STEP 3: Convert Result to Output's Unit

104 --> No Conversion Required

FINAL ANSWER

104 <-- Deviation of Main Undercarriage

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Civil » Transportation Engineering » Airport Planning and Design » Taxiway and Exit Taxiway Design » Taxiway Design » Design of Fillets » Maximum value of Deviation of main Undercarriage given Radius of Fillet

Credits

Created by Mithila Muthamma PA

Coorg Institute of Technology (CIT), Coorg

Mithila Muthamma PA has created this Calculator and 2000+ more calculators!

Verified by Chandana P Dev

NSS College of Engineering (NSSCE), Palakkad

Chandana P Dev has verified this Calculator and 1700+ more calculators!

< 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

Maximum value of Deviation of main Undercarriage given Radius of Fillet Formula

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

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 Maximum value of Deviation of main Undercarriage given Radius of Fillet?

Maximum value of Deviation of main Undercarriage given Radius of Fillet calculator uses Deviation of Main Undercarriage = -(Radius of Fillet-Radius of Taxiway Centerline+Minimum Safety Margin+(Track of Main Undercarriage/2)) to calculate the Deviation of Main Undercarriage, Maximum value of Deviation of main Undercarriage given Radius of Fillet is defined maximum value when datum point has covered distance along straight segment of guideline, for assumed steering angle. Deviation of Main Undercarriage is denoted by γ symbol.

How to calculate Maximum value of Deviation of main Undercarriage given Radius of Fillet using this online calculator? To use this online calculator for Maximum value of Deviation of main Undercarriage given Radius of Fillet, enter Radius of Fillet (r), Radius of Taxiway Centerline (R), Minimum Safety Margin (M) & Track of Main Undercarriage (T) and hit the calculate button. Here is how the Maximum value of Deviation of main Undercarriage given Radius of Fillet calculation can be explained with given input values -> 104 = -(27.5-150+15+(7/2)).

FAQ

What is Maximum value of Deviation of main Undercarriage given Radius of Fillet?

Maximum value of Deviation of main Undercarriage given Radius of Fillet is defined maximum value when datum point has covered distance along straight segment of guideline, for assumed steering angle and is represented as γ = -(r-R+M+(T/2)) or Deviation of Main Undercarriage = -(Radius of Fillet-Radius of Taxiway Centerline+Minimum Safety Margin+(Track of Main Undercarriage/2)). 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, 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 & 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.

How to calculate Maximum value of Deviation of main Undercarriage given Radius of Fillet?

Maximum value of Deviation of main Undercarriage given Radius of Fillet is defined maximum value when datum point has covered distance along straight segment of guideline, for assumed steering angle is calculated using Deviation of Main Undercarriage = -(Radius of Fillet-Radius of Taxiway Centerline+Minimum Safety Margin+(Track of Main Undercarriage/2)). To calculate Maximum value of Deviation of main Undercarriage given Radius of Fillet, you need Radius of Fillet (r), Radius of Taxiway Centerline (R), Minimum Safety Margin (M) & Track of Main Undercarriage (T). With our tool, you need to enter the respective value for Radius of Fillet, Radius of Taxiway Centerline, Minimum Safety Margin & Track of Main Undercarriage and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

Home

FREE PDFs

🔍 Search