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This wing area calculator allows you to compute the wing area for different types of aircraft wing designs. You can select between three types of wing shapes: rectangular, trapezoidal, and elliptical. The calculator uses the appropriate formula based on your selection and inputs the wingspan and chord measurements.
The following are the formulas used to calculate the wing area for different wing shapes:
A = b × c
b
is the wingspan and c
is the mean chord (average width).
A = (b × (c_root + c_tip)) / 2
b
is the wingspan, c_root
is the root chord, and c_tip
is the tip chord.
A = (π / 4) × b × c
b
is the wingspan and c
is the mean chord.
Here’s an example of how the calculator works for a rectangular wing:
This process is similar for other wing shapes, though the formulas differ slightly depending on whether the wing is rectangular, trapezoidal, or elliptical.
A rectangular wing has a consistent chord (width) from the root to the tip. This type of wing is simple and easy to calculate, making it common for many basic aircraft designs.
A trapezoidal wing has a wider root chord (near the aircraft body) and a narrower tip chord (at the wingtip). This type of wing design is often used for better aerodynamic performance and more efficient lift distribution.
An elliptical wing is shaped like an ellipse, providing smooth airflow and efficient lift distribution. This type of wing is often seen in more advanced and high-performance aircraft.
The wing area is crucial for determining the amount of lift an aircraft can generate. Larger wings typically generate more lift, which is essential for supporting the weight of the aircraft during flight.
Yes! The calculator can be used for various aircraft types, as long as you know the wingspan and the chord measurements. Different wing shapes are commonly used in both small and large aircraft.
This calculator is based on the information from the NASA Glenn Research Center Virtual Aero website. The formulas and explanations for different wing shapes have been adapted from their educational resources.