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Old May 26th 11, 02:20 AM posted to rec.aviation.piloting
Dudley Henriques[_3_]
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Default Lift - Newton/Bernoulli ratio...

On May 25, 6:55*pm, Dave Doe wrote:
In article 47971036-2b4d-4297-bcbf-
, ,
Dudley Henriques says...











On May 25, 2:36 am, Dave Doe wrote:
In article 6469c134-67e0-4ca9-8dd1-
, , a says....


On May 24, 10:35 am, Dudley Henriques
wrote:
On May 23, 9:31 pm, a wrote:


On May 22, 10:02 pm, brian whatcott wrote:


On 5/22/2011 5:15 AM, Dave Doe wrote:


Does anyone have any figures and references for about what ratio lift is
produced by Newton's Laws and Bernoulli's Laws?


I appreciate this is not a static figure - but say a yer average C-172,
or perhaps a 737.


I would hazard a semi-educated guess that lift is *primarily* produced
by angle of attack (or deflection if you like) - Newton's Laws - and by
a much lesser degree by Bernoulli's Law. I would guess that Bernoulli's
principle might create 20% of the lift a wing generates. A friend
believes it would be much lesser - about 5%.


Think of it this way:
Newton: force is proportional to the mass and its acceleration.