What Is Lateral Stability And How It Affects The Aircraft In Flight? Stability about the aircraft’s longitudinal axis, which extends from the nose of the aircraft to its tail, is called lateral stability. Positive lateral stability helps to stabilize the lateral or “rolling effect” when one wing gets lower than the wing on the opposite
What Are The Effects Of A Aft CG? With the CG aft, the aircraft will have a lower stall speed due to decreased wing loading. The aft CG will cause the elevator and rudder to be less effective. This is because the arm from the CG to the elevator and rudder is shorter. Which is
What Causes Dutch Roll? Answer: Dutch roll is a natural aerodynamic phenomenon in swept-wing aircraft. It is caused by the design having slightly weaker directional stability than lateral stability. The result is the tail of the airplane seeming to “wag” or move left and right with slight up and down motion. Why is it called
What Gives The Aircraft Directional Stability? Yawing or directional stability is the most easily achieved stability in aircraft design. The area of the vertical fin and the sides of the fuselage aft of the CG are the prime contributors that make the aircraft act like the well known weather vane or arrow, pointing its nose