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Develop runway structures (for both flexible and rigid) for the airport that will serve the following aircraft for the next 20 years. Aircraft B737-600 B767-200

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Develop runway structures (for both flexible and rigid) for the airport that will serve the following aircraft for the next 20 years. Aircraft B737-600 B767-200 A320-100 A330-300 std Gross Weights (lbs) 146,000 361,000 150,796 509,047 Annual Departures 1,460 1,460 1,825 730 1) Design life: 20 years with 2 % annual growth in aircraft operations 2) All the other features of aircraft (tire pressure, tire contact length and width, area, or other features) are as specified in the given example in FAAFIELD program. 3) Resilient modulus of subgrade in this area is 11,000 psi. Default modulus values are to be used for the other layers. For rigid runway structure, determine the slab thickness with the use of the sublayers of 6-in P304 cement treated base and 8-in P209 crushed aggregate base. For flexible runway structure, determine the required thickness of P209 crushed aggregate base, when 6-in P401/P403 surface layer with 5-in P401/P403 HMA stabilized base are used. Also, discuss which aircraft contribute most in cumulative damage. Develop runway structures (for both flexible and rigid) for the airport that will serve the following aircraft for the next 20 years. Aircraft B737-600 B767-200 A320-100 A330-300 std Gross Weights (lbs) 146,000 361,000 150,796 509,047 Annual Departures 1,460 1,460 1,825 730 1) Design life: 20 years with 2 % annual growth in aircraft operations 2) All the other features of aircraft (tire pressure, tire contact length and width, area, or other features) are as specified in the given example in FAAFIELD program. 3) Resilient modulus of subgrade in this area is 11,000 psi. Default modulus values are to be used for the other layers. For rigid runway structure, determine the slab thickness with the use of the sublayers of 6-in P304 cement treated base and 8-in P209 crushed aggregate base. For flexible runway structure, determine the required thickness of P209 crushed aggregate base, when 6-in P401/P403 surface layer with 5-in P401/P403 HMA stabilized base are used. Also, discuss which aircraft contribute most in cumulative damage

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