PILOT GLIDER WRITTEN EXAM LATEST ACTUAL EXAM 553 QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED ANSWERS) | ALREADY GRADED A+ Question 1 The term "angle of attack" is defined as the angle between: --ANSWER>>>: The wing chord line and the relative wind Rationale: Angle of attack is a fundamental aerodynamic concept that determines the lift coefficient of an airfoil. It is measured between the chord line (an imaginary straight line from the leading edge to trailing edge) and the relative wind (the direction of the airflow relative to the wing) . Question 2 The angle between the chord line of an airfoil and the relative wind is known as the angle of: --ANSWER>>>: Attack Rationale: This is the formal definition of angle of attack, which is critical for understanding lift generation and stall characteristics in glider flight . Question 3 What actually makes a glider fly? --ANSWER>>>: The special shape of the wing creates a suction effect above the wing and a pressure effect below the wing, generating lift Rationale: The curved upper surface of a glider's wing causes air to accelerate, reducing pressure above the wing while higher pressure below creates net upward lift. When sufficient lift is generated, the