How does drag change with Reynolds number?
Recall the definition of the Reynolds number:



Where &rho; is the density, v is the velocity, &mu; is the viscosity of air and l is the characteristic length.

The characteristic length is typically the chord length of an airfoil but can also mean the overall length of the airframe. When we scale down a model, we are decreasing l.

Decreasing l while holding all other variables constant (which I assume is what you meant about "forgetting to adjust the Reynolds number"), has the net effect of lowering your Reynolds number.

Looking at airfoil graphs for example, we can see the relationship between the Reynolds number and the drag coefficient of the body:



It is obvious from the graph that the drag coefficient increases when the Reynolds number is lower (higher curve on the graph)

Image source: Airfoil tools