for setting up the plane you talk first of elevators then ailerons I am assuming they are the same?
Also you say the same can be said about the rudder, what do you mean?
This is worth clarifying. The ailerons are on the outermost point of the wing. They move opposite to each other. They cause a plane to bank from right to left and left to right. The rudder controls the planes Yaw motion. that is, left to right, right to left, no banking (thought in reality, when you Yaw a plane, the wing in front will cause the plane to lift that wing first and the plane will bank, if not cancelled out by the ailerons. A well balanced plane would have the rudder and ailerons capable of cancelling each other out).
The elevator(s) move in unison. The nose the plane up and down.
In a glider, if you have to adjust the rudder, that usually means a flaw in the build, a twisted fuselage or wings that are not exactly symmetrical, or a rudder that is not on an exact center line with the fuselage and not located correctly to the wings. If you have to adjust the rudder in a paper model, it will probably never fly decently, because of the drag, and the fact that it will constantly be changing the yaw of the craft.
The Center of gravity should always be done statically. On a Delta wing aircraft, their is a tendency for them to nose up if thrown hard and sometimes the elevators must be pointed slightly down.
This aircraft actually used what was called "elevons" a combination of elevator and ailerons. They could function as both. This was necessary for a lot of reasons, and books have been written on it, but basically, in a pure Delta wing craft, when a pilot pulls back on the stick, the trailing edge loses all lift, while the leading edge still has lift, the plane then noses up. This could, and often did, lead to bad situations where the planes would stall on take off or landing. They needed really long runways to overcome this, and subsequently needed a more robust landing gear.
Trimming a delta winged aircraft for level flight causes the wing to create a massive amount of drag. This is why this style wing has fallen into obsolescence, unless a canard is used up front. This of course excludes the "cranked" delta wing, which has a completely different set of aerodynamics.
Since a glider is usually climbing, then returning, a Delta wing glider can successfully be trimmed for this, achieving great height, then a safe landing. it is hard to make one "hang" in the air though, compared to the same amount of lift area on a conventionally shaped wing, or a wing with the planform of a conventional glider.
