Krueger flaps Calculator

The formula for calculating the increase in lift coefficient due to Krueger flaps can be quite complex and depends on various factors such as flap deflection angle, wing geometry, and aircraft speed. However, a simplified formula commonly used is:

Where:

  • is the increase in lift coefficient
  • is a constant related to the effectiveness of the Krueger flaps
  • is the angle of attack
  • is the efficiency factor of the Krueger flaps

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