You just need max L/D and best glide speed
A quick look. Short version. L/D max = 10 at best glide speed of 85 mph. TV = sqrt L/D max X best glide speed. Then double L/D, keep 85.
TV = sqrt of (10 or 20) X 85 = 270 to 385 mph
plug in the correct values for your airplane
Long version. Start with L/D max of 10 at best glide speed of 85 mph. For L/D, L=W and for TV, D=W, so starting with the drag at the max L/D speed, D has to increase by a factor of 10 (L/D max) to equal W which you get by increasing speed by a factor of (sqrt 10). Keep all things the same (configuration, stick position?.), then TV = sqrt (L/D max) X best glide speed, or =sqrt 10 X 85 (or about 3 times best glide speed). Of course the wing would have to produce 10 Gs at an L/D of 10 and would separate before reaching TV. That would count as a change in configuration. So lets look at zero lift even though there is still no guarantee that the wings would stay on. Since cd=cdo+cdi and at max L/D and best climb speed, cdo=cdi or cd= 2 X cdo. A zero lift situation gives a cd = cdo or ? the D in the 10 L/D noted above. With ? drag, our L/D would double. We?ll cheat here a little bit. Just plug 20 into the L/D max knowing that L is 0, keep the 85. So a zero lift TV = sqrt 20 X 85 (about 4.4 times best glide speed). Therefore, TV by calculation is 272 pulling 10 Gs or 385 pulling 0 Gs.
Sometimes all we need to know is what the answer isn?t. It isn?t likely that we can fly our RVs at 272 pulling 10 Gs or 385 at 0 Gs, so we don?t need to be very precise since we are now dealing with a theoretical speed.
Also, the speeds are indicated rather than true. At altitude, you would need to convert to true. Just think, a TV at 20,000 feet is 37% greater than TV at SL. It is good to know that once reaching TV, you would be slowing down when you hit the ground at 385 mph. That is when you would experience terminal acceleration. Terminal acceleration is more of a social or physiological issue rather than an engineering issue, so I won?t try to explain that one further.