Question: 1. Consider an aircraft designed for a positive limit load factor of 3.5. a) What is the structurally safe minimum radius of a symmetric

1. Consider an aircraft designed for a positive limit load factor of

1. Consider an aircraft designed for a positive limit load factor of 3.5. a) What is the structurally safe minimum radius of a symmetric pull out that the aircraft can execute at a dive speed of 350 m/s? 5 marks b) What is the structurally safe minimum turn radius R at which the aircraft would be able to execute a correctly banked turn at an airspeed of 180 m/s? 5 marks

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