Question

Corner point in the \(V\)-\(n\) diagram is

• A. Maximum velocity
• B. Stall limit meets structural limit
• C. Lift equals weight
• D. Drag is in maximum condition

Hint:

The corner point of the \(V\)-\(n\) diagram is also called the \[ \boxed{\text{Maneuvering Speed }(V_A)} \] where the aircraft reaches the structural load limit exactly at stall.

Answer 1

The Correct Option is B

Step 1: Recall the \(V\)-\(n\) diagram. The \(V\)-\(n\) diagram represents the relationship between \[ \boxed{\text{Airspeed }(V)} \] and \[ \boxed{\text{Load Factor }(n).} \] It is also known as the flight envelope.

Step 2: Identify the corner point. The corner point is the point where \[ \boxed{\text{the stall boundary intersects the structural load limit}.} \] This represents the highest load factor that can be achieved before the aircraft stalls. Therefore, \[ \boxed{\text{Stall limit meets structural limit}} \] is the correct answer. Thus, \[ \boxed{(B)} \] is the correct answer.