Hi Allan,
It is very possible the Cosmic Wind is tail heavy. The airplane is a little unique in that all the taper (and there's quite a bit of it) is in the trailing edge. This has a very real aerodynamic impact. It in essence makes the nose shorter by virtue of moving the center of lift forward.
But don't get bogged down in the aero details because the solution is much simpler. The Center of Gravity has to be located in the correct position based on the Mean Aerodynamic Chord (MAC). Again, don't worry about the terminology. This is simply the way the engineer designers looks at the wing shape and area to determine where the lift will be generated with respect to the length of the overall airplane. Again, don't worry about the technicalities.
The solution is to locate your CG in the correct position on the MAC. It's simple and here's how to do it. (By the way, this explanation will be simplified because we're going to use the "AVerage" chord instead of the slightly more difficult to determine MAC. For a simple tapered wing and stunt aerodynamics this is more than adequate.
First measure from the center of the fuselage to either wing tip. Lets just say that is 22 inches. Divide that in half and you come up with 11 inches. Locate that 11 inch location and mark it.
Now mark a temporary straight line, parallel to the fuselage, from the leading edge to the trailing edge at that point.
Measure that distance. Just for example purposes let's say that distance is eight inches.
Now, because the Cosmic Wind is a flapless design I'm going to suggest that you locate your Center of Gravity at a point 15% aft of the Leading Edge at that "halfspan" location. So you multiply the chord (8") times 15% (.15) and the result is 1.2". This is where the CG should be located, 1.2" aft of the leading edge. (NOTE: Because your wing has a straight leading edge, with all the taper in the trailing edge, you can measure that 1.2" anywhere on the wing. This is very convenient because you can go all the way out to the wingtips, make a mark on both wingtips 1.2" aft of the leading edge.
Now add or subtract weight at the nose or tail until the airplane balances with a finger tip held at each of those marks at the tips. I guarantee you that this will be an excellent starting place for the CG on an unflapped ship like your C.W.
Set the CG at that point and fly the airplane a few times and then, if necessary, make the adjustments to the handle and control system that Denny suggested above. Doing so will result in a ship trimmed within a fraction of inch of the optimum center of gravity.
ONE BIG CAUTION. THE ABOVE NUMBERS (15% PRIMARILY) ARE NOT NECESSARILY APPROPRIATE FOR FLAPPED DESIGNS ALTHOUGH USING 15% WILL ALWAYS RESULT IN A FLYABLE RESULT. The reasons why are a little complex but not germane to Al's predicament.
Ted Fancher
p.s. just noted your later comments on the muffler. Yes, definitely take the weight off the tail and most likely go ahead and mount the muffler. Then check the CG as described above and adjust accordingly.