2000xp8 said:
Which numbers do you find to be more relevant? I guess there's real world numbers and bench numbers. But on the first page of the article it says "naturally testing included time on the flow bench".
Done
28 inches (which i hope you will explain to me).
Joe
They don't say how the flow numbers were done - head alone like the numbers in the table? Probably, but we don't know cause they didn't say - but we can surmise that maybe by looking at Parts I & III. However, the .450" lift peak flow number was 187cfm - the table you said has been proven wrong indicates about 195 cfm - well within normal variances for casting differences and bench set up/operator variances for flow testing - 7cfm. Also note that the valve lift height where the peak flows were taken was changed - taken @ .450" lift for the E7 and P heads and .550" lift for all the others, but a table with .500" lift was given on page 184 in Part II as well as Part I.
Note: MM&FF @ .500", table taken @ .500"
E7 peak - 157cfm MM&FF, 155cfm table
GT40P - 185 cfm MM&FF, 195 table
Windsor Jr - 203cfm MM&FF, 186cfm table
GT40Y - 206cfm MM&FF, 213cfm table
Canfield - which Canfiled in the table is not given, so can't really compare
Brodix - 239cfm MM&FF, 243cfm table
Systemax - 237cfm MM&FF, table 219cfm
Performer - 234cfm MM&FF, table 214cfm
AFR 165 - 237cfm MM&FF, table 250cfm
These variances are not huge and are actually within the variances that you find on the referenced websites when comparing flow test done by others posted there. These variances, like I said, are due to manufacturing variances as well as test bench/set up variances. Is that enough variance to say the table in Stangnet is discredited and should not be used?
28" of water depression indicates the intake vacuum level used during the test. A manometer is used which is a long clear tube attached to a scale that has inches marked on it like a ruler. The clear tube has red colored water in it and when attached to the vacuum in the manifoild pulls the water up 28". You can see that in Part I and Part III.