Earlier, ET wrote:

Here's one: www.nexaer.com

That wing/fuselage junction looks pretty draggy, with the fuselage
sweeping up right where the trailing edge meets the fuselage. I wonder
if they've done any analysis of the airflow in that area.

I'd think that with the frontal area of their 54" wide cabin (that's
what, 10" wider than a Grumman 2-seater?), they'd want to take every
opportunity to keep the overall drag down.

Bob K.