Had similar problem on my RV-4 and I took a different less draggy approach. I put to VG's in front of the NACA scoop.
The two NACA inlets where in my canopy skirt on RHS. A combo of the Prop corkscrew, slip stream, laminar airflow, the
air coming into cockpit was weak. After the VG Mod I had good to very good flow. Also consider cockpit exit air flow scoop.
NACA Scoop
............VG's (angle not as shown, less acute)
_______
I
..........( _____
............\
I
......................(___
.......\
I
..................... ___I
I
............_____(
............./
I______(
....................../
I had all the dimensions and angles written down long ago. I recall I posted something. It worked great. My text sketch above
is not accurate; the angle of the VG's was more aligned with airflow. I recall VW's were 1 to 1.5" long and standard height about 3/8".
They were about 1/4" to .5" fwd of fwd edge if scoop, with a VG angle of about 20-30 degrees to airflow, with the outer edge aligned
with the outer edge of the aft end of the NACA scoop. They were temporary taped on and played with many angles and position. It
was night and day difference, when I hit on the right combo. Once the VG's were dialed in, I don't recall if bonded them on with tank
sealant or used two way sticky tape the VG's had. I do recall they were there 6 years later when I sold the airplane.
What you did is make this more of a standard scoop into free air stream. This works well but does add drag. I'm surprised you even
see 1 MPH. That is well inside the margin of error. Flight testing in standard smooth conditions from one day to the next is hard to do.
Nice work... I like it. If it works cool (pun intended). If you want to experiment I think it would be cool if you try the VG idea as well.
See if you can further the air flow (or not and just enjoy flying

).