To calculate wing loading, divide the mass of the bird or plane by the total area of the upper surface of its wings: wing loading = body mass (kg)/wing area (m2).

## How do you calculate wing load distribution?

Wing load lift Assuming an elliptical distribution for lift across the length of the wing, resulting in the following expression for lift profile: q1(x) = ka √L2 – x2; where L = length of wing; x = position along wing; and ka = lift profile coefficient.

Power loading, the ratio of airplane’s weight to engine power output, is determined by dividing a propeller-driven airplane’s current weight by the engine’s generated horsepower (hp). For a jet-powered airplane, power loading may be determined as pounds of weight per pounds of jet thrust.

Murres. Although flight is energetically costly for murres, their high wing loading (the highest of any flying bird; Livezey, 1988) allows them to fly very fast.

### What is wing load factor?

In aeronautics, the load factor is the ratio of the lift of an aircraft to its weight and represents a global measure of the stress (“load”) to which the structure of the aircraft is subjected: where is the load factor, is the lift. is the weight. Since the load factor is the ratio of two forces, it is dimensionless.

At Mach 0.85 and 0.7 lift coefficient, a wing loading of 50 lb/sq ft (240 kg/m2) can reach a structural limit of 7.33 g up to 15,000 feet (4,600 m) and then decreases to 2.3 g at 40,000 feet (12,000 m).

The power loading of the aircraft is maximum gross weight divided by the chosen rated power. Note that a low power loading value corresponds to an aircraft with a more powerful engine and/or a lower gross weight. Low power loading means better performance.

How To Calculate WCL

1. Divide the Wing Area measured in Square Inches by 144.
2. Raise the result of Step 1 to the power of 1.5.
3. Find the Takeoff Weight in Ounces of your airplane. This includes fuel if applicable and batteries and divide that by the result of Step 2.

To compensate, the lift force must be increased by increasing the angle of attack by use of up elevator deflection which increases drag. Turning can be described as ‘climbing around a circle’ (wing lift is diverted to turning the aircraft) so the increase in wing angle of attack creates even more drag.

### How is load factor calculated?

Load factor is a measurement of the efficiency of your household’s electrical energy usage. It is calculated by taking the total electricity (kWh) used in the month, divided by your peak demand (kW) multiplied by the number of days in the billing cycle and the total hours in a day.

### What is the ratio of load factor?

Definition: Load factor is defined as the ratio of the average load over a given period to the maximum demand (peak load) occurring in that period. In other words, the load factor is the ratio of energy consumed in a given period of the times of hours to the peak load which has occurred during that particular period.

How to Calculate the Wing Loading of a Flying Model Aircraft The wing loadingof an aircraft is the measure of weightcarried by each given unit of area. For model aircraft, wing loading is expressed as ounces per square foot(oz./ft2). Experience with different models will make this figure more meaningful to you.

## How much does a F-16 fly by wire weigh?

The General Dynamics Case Study on the F-16 Fly-By-Wire Flight Control System. AIAA Professional Study Series. 4/21/04 13 Performance •Empty Weight – 16,285 lb •Combat Takeoff – 26,536 lb •Maximum Takeoff Weight – 37,500 lb •Wing Loading – 88 lb/ft2 •Maximum Thrust – 23,830 lb (27, 000 lb for later models) •Thrust/Weight Ratio – 0.94-1.08

## How does the F-16 work?

The F-16 has a head-up display (HUD), which projects visual flight and combat information in front of the pilot without obstructing the view; being able to keep their head “out of the cockpit” improves a pilot’s situation awareness. Further flight and systems information are displayed on multi-function displays (MFD).

How many G’s can the F-16 withstand?

With a full load of internal fuel, the F-16 can withstand up to nine G’s — nine times the force of gravity — which exceeds the capability of other current fighter aircraft. The cockpit and its bubble canopy give the pilot unobstructed forward and upward vision, and greatly improved vision over the side and to the rear.