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F-22 & CF-105 Flight Performance Simulation
Jose A. Perez F-22 & CF-105 Flight Performance Simulation Aero 211 Bonus Project
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F-22 Capabilities: Highly maneuverable ground attack, electronic warfare signals intelligence roles Cost: $138 million
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F-22 Specification: S= Wing Area= 840 ft^2 b= Wing span= 44.5 ft. W= Take-off Weight= lb. e= Oswald efficiency factor= 0.82 Wfuel= Fuel Weight= 2600 lb. ct= Thrust Specific Fuel Consumption= 0.8 lb/(lb. thrust*h) Ttakeoff= Take-off Thrust= lb T= Total Thrust= lb CDo1= Drag Coefficient= 0.015
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CF-105 Capabilities: delta-wing interceptor aircraft, Designed for supersonic flights intercept and destroy enemy aircraft. Cost: $164 million
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CF-105 Specification: S= Wing Area= 1225 ft^2 b= Wing span= 50 ft. W= Take-off Weight= lb. e= Oswald efficiency factor= 0.75 Wfuel= Fuel Weight= 8000 lb. ct= Thrust Specific Fuel Consumption= 0.8 lb/(lb. thrust*h) Ttakeoff= Take-off Thrust= lb T= Total Thrust= lb CDo1= Drag Coefficient= 0.016
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F-22 F-22: Max. Velocity=6638 ft/sec Range = *10^8 ft Endurance = hours F-22 Model: Max. Velocity= ft/sec Range = ft. Endurance = minutes
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CF-105 CF-105 Max. Velocity= ft/sec Range = *10^6 ft. Endurance = hours CF-105 Model Max. Velocity= ft/sec Range = ft. Endurance = 1.39 minutes
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