Angle of attack is
the angle between the flat ground and the cord of the airfoil.
Airfoil is the
cross section of the wing parallel the plane.
Lift is the amount
of upward force that is produced from the angle of attack, thrust, area
of the wing and shape of the air foil.
Drag is the amount
of force acting against the aircraft in the horizontal axis on the
plane.
Weight is the total
mass of the aircraft (and everything in it) multiplied by gravity (32.2
ft/s2).
Thrust is the
amount of forward force acting in the horizontal axis of the aircraft.
This force comes from the aircrafts power plant and is usually either a
prop engine and is measured in HP, or a turbine engine measured in KW.
Planform
Area is basically described as the area of the wing.
Angle of attack and Outline of an Airfoil
http://www.researchsupporttechnologies.com/boomerang_site/Boomerang
aerodynamics3_files/angle of attack.jpg