The static stability of an aircraft depends primarily on:

More from Flight Mechanics MCQ:

• Which of the following is the correct expression for Lift (L)?
• The drag polar of an aircraft relates:
• The angle of attack is defined as:
• The condition for level unaccelerated flight is:
• The load factor (n) in flight mechanics is defined as:
• Which point is the effective point of action of aerodynamic forces?