Okay "taper" wasn't the technically correct term to use, I just prefer to keep it to more broadly understandable language on public forums. What I mean is that for a profile with the same leading section, a truncated airfoil that terminates in a narrower trailing edge is faster at low yaw, so effectively a lower aspect ratio airfoil.
The problem with desiging a head tube is that you have to fit things inside, so you don't have too much freedom in designing the leading section. Ideally, you'd probably place the steerer closer to the middle of the head tube (Pinarello Bolide F TT), to give you more freedom in design. I placed the steering axis 45 mm behind the front edge of the head tube. I can't say with any true certainty, but I think that's on the far side of the spectrum compared to most of what's on the market.
Yesterday I took the widest leading section of my HT design (a 45 and 26 mm radius half ellipse), and ran cfd tests with trailing edges of the same lengths and different width trailing edges. I tested the 38mm I originally used, 28, 20, 15 and 10mm (and a 2 mm radius fillet on all of them) at 40 and 50 kmh from 0 to 12°. As the trailing edge narrowed, the result was consistent improvement at low yaw and, conversely, deterioration at rising yaw.