Wing Area Given By Tail Area Calculator

Wing area is the total surface area of an aircraft’s wings that is exposed to the oncoming air during flight. It is a critical parameter in determining the aerodynamic characteristics and performance of an aircraft. Wing area is typically measured in square units, such as square feet or square meters, and it plays a key role in the generation of lift, the production of drag, and the overall maneuverability of the aircraft. The formula to calculate Wing area as follows:

Where:

  • S is the wing area in m2.
  • Qw is the Wing dynamic pressure in Pa.
  • Cn is the  Yawing moment coefficient.
  • lv is the Vertical tail moment arm in m.
  • Sv is the Vertical tail area in m2.
  • Cv is the Vertical tail Lift curve slope in 1/rad.
  • β is the Sideslip angle in radian.
  • σ is the Sidewash angle in radian.
  • Qv is the Tail Dynamic pressure in Pa.
  • b is the wingspan in m.

Leave a Comment

Your email address will not be published. Required fields are marked *

Scroll to Top