| If you think about it, there are the same number of bends regardless of whether it is a FMIC or SMIC. So much for your big "U" theory. 2nd of all? Are you kidding? The charge airflow numbers are *much* better for side mounts, because they have a much bigger flow area. Do the math. Your UAS front mount has a charge flow area of 3.5" x 6", whereas Stillen has 3.5" x 9.4". Which has more area? Not to mention the UAS core is 24" long, which will cause more resistance to flow. Each core on the UAS FMIC flows 183 cfm at 1.5 psi pressure drop. Each Stillen flows 332 cfm at the same pressure drop. Please...am I missing something here? If you've got test data to refute what I'm saying I'd *love* to see it...
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