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Null Hypothesis 1: If the chamber of the airfoil is greater, then the lift of the aircraft will also be greater Null Hypothesis 2: If the chord line of the airfoil is longer, then the lift of the aircraft will be greater Null Hypothesis 3: If the thickness of the airfoil is increased, then the lift of the aircraft will also increase
by simscalesimscale
kalemao createdthis project
almost 6 years ago
kalemao copied this project
almost 6 years ago