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Search: Posts Made By: cl12pv2s
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Forum: Rotorheads
8th May 2006, 08:48
Replies: 95
Views: 17,837
Posted By cl12pv2s

Crab, Yes, It was indeed...but I think he...

Crab,

Yes, It was indeed...but I think he was just being sloppy and really meant 'an increased conponent from below'!

While I'm here, I may as well look into what Dave said...


Dave you...
Forum: Rotorheads
7th May 2006, 17:10
Replies: 95
Views: 17,837
Posted By cl12pv2s

Nick, While FanPilot seems to be very happy...

Nick,

While FanPilot seems to be very happy to slap his own back, I would go so far to say that I can see your point about the AoA on the horizontal stab (I admit I didn't see it from that angle...
Forum: Rotorheads
7th May 2006, 05:12
Replies: 95
Views: 17,837
Posted By cl12pv2s

TC, No one is disagreeing that the change in...

TC,
No one is disagreeing that the change in magnitude is differerent.

Just wondering if you agree with this statement?

"With respect to the following formula [Lift = 1/2 x rho x v squ'd x S x...
Forum: Rotorheads
3rd May 2006, 11:03
Replies: 95
Views: 17,837
Posted By cl12pv2s

Thomas, This doesn't seem to be the case...

Thomas,

This doesn't seem to be the case when I run the numbers through a simple 'lift formula' spreadsheet. A change of pitch doesn't appear to change the ratio of lift between the adv and rtg...
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