A stopped prop is in a complete stall
condition, and would be expected to provide less drag than one that is turning
at an RPM of incipient stall. There will be some RPM for a given pitch
and touchdown speed that will provide the most drag. We just have to
figure out what that is.
Landing speed in Kts times 100 gives you
ft/min. Pitch divided by 12 gives you ft/min per revolution of the prop
for neutral thrust (approx.). So my 85 pitch prop at 70 kt landing speed
is neutral at 1000 RPM. So maybe the max drag point is somewhere
around 650 RPM (mas o menos 100). Just a guess. Someone less propeller-design
challenged than I may have a better answer.
Al