Aircraft weight divided by wing area
Expression for the weight per unit wing area of a model.
ratio of wing area to weight carried in flight. Determined by dividing glider's total wing area by the combined weight of pilot, glider and all gear that will be carried in flight.
Wing loading is the weight of the aircraft divided by the wing area. It is designated ounces per square foot.
This is the amount of weight per square foot that has to be overcome to provide lift. It is normally expressed in ounces per square foot. This specification can be easily calculated as follows: If you know the square inches of the wing, simply divide by 144 to obtain square feet. Divide the total weight (in ounces) of the airplane by the wing area (in square feet). This information is valuable when deciding on which airplane to build next. Planes with high wing loading numbers must fly faster to stay in the air. These are generally "performance" airplanes. Conversely, planes with lower numbers do not need as much air flowing around the wing to keep it flying. Gliders and trainer airplanes fall into this category because slow, efficient flight is desirable.
The weight of an aircraft divided by the area of the wing produces a wing loading figure such as 1lb/sq foot.
ratio of weight to wing area. Lower wing loading permits slower flight without stalling.
The ratio of weight born by a wing to its surface area. In the US, divide your exit weight in pounds by the square footage of the canopy. The Letter XYZ
In aerodynamics, wing loading is the loaded weight of the aircraft divided by the area of the wing. It is broadly reflective of the aircraft's lift-to-mass ratio, which affects its rate of climb, load-carrying ability, and turn performance.