A-14A Wild Wolf

Has a 30mm Minigun called the GAU-8 as it primary weaponry.

It can hold the latest of the AIM-9 series of Missiles and long range air to air missiles like AIM-260 JATM, and the latest generation of Air to Ground missiles, Guided or Unguided bombs, Laser Guidance Systems

16.50 Meters

18.40 Meters

Has 6 Wing Plyons that can hold all secondary weaponry.

A Inner Missile/Bomb bay located in the middle of the aircraft that has 3 plyons

Is the successor of the Fairchild Republic A-10 Warthog and is a 5 generation attack aircraft. On reality it never even made out of basic sketches.

The A-14A Wild Wolf unlike it's predecessor will have stealth characteristics

The A-14A Wild Wolf doesn't bare any consciousness, it is only a prototype attack aircraft.

Lift is generated by an Airfoil(The Wing of an given aircraft) by generating low pressure under the curvature of the wing, and high pressure over the wing. The magnitude of the force acting over a small section of an object immersed in a fluid equals the pressure p times the area A of the section. A quick units check shows that:

p * A = (force/area) * area = force

As discussed on the fluid pressure slide, pressure is a scalar quantity related to the momentum of the molecules of a fluid. Since a force is a vector quantity, having both magnitude and direction, we must determine the direction of the pressure force. Pressure acts perpendicular (or normal) to the solid surface of an object. So, the direction of the force on the small section of the object is along the normal to the surface. We denote this direction by the letter n.

The normal direction changes from the front of the airfoil to the rear and from the top to the bottom. We indicate this variation on the figure by several small arrows pointing perpendicular to the surface and labeled with an n. To obtain the net mechanical force over the entire solid object, we must sum the contributions from all the small sections. Mathematically, the summation is indicated by the Greek letter sigma ( ) The net aerodynamic force F is equal to the sum of the product of the pressure p times the incremental area delta A in the normal direction n.

F =   p * n * delta A

In the limit of infinitely small sections, this gives the integral of the pressure times the area around the closed surface. Using the symbol S dA for integration, we have:

F = S (p * n) dA

where the integral is taken all around the body. On the figure, that is why the integral sign has a circle through it.

If the pressure on a closed surface is a constant, there is no net force produced because the summation of the directions of the normal adds up to zero. For every small section there is another small section whose normal points in exactly the opposite d