OK so what did the testing show? Below is the testing I did and the results.
I used a digital tach, amp meter between the battery and ESC, and a digital scale that measured the pull from the plane.
Test 1
Prop Revs Current @ battery Thrust measured by pull test
12x6.5WEP 8100 32amps, 475 watts 56 ounces (well below the all up weight of 62 ounces)
1 minute motor run used 23% of battery and recharged with 594mha.
Using the formula (594x5) x (.70) x(1.2)=2495mha for a 5 minute run. I have used this formula many times and it is fairly accurate
for predicting flight usage. This is well withing the 2600mha pack I plane to use.
------------------------------------------------------------------------------------------------------------------------------
Test 2
12x6EP 9000 36amps, 512 watts 61 ounces (almost equal to the all up weight of 62 ounces)
1 minute motor run usage 28% of battery and recharged with 625mha.
Using the formula (625x5) x (.70) x (1.2) = 2625Ymha for a five minute flight. It's just outside the 2600mha battery, but a slight reduction in revs
could correct that.
Test 3
I reduced the revs on the 12x6EP to where the thrust was equal to the 12x6.5WEP @ 8100 RPM. The system developed 56 ounces at 8700RPM with a
current draw of 33amps at 480 watts. In short when the two props were compared just using generated thrust they compared equally or at least within the margin of error for my tach, amp meter and digital scale used to make the measurement.
Andy