limit of trim = limit of travel?

On May 8, 4:44 pm, nospam wrote:

What I wrote totally contradicts your claim that the functions of the
components of an aircraft tail cannot be separated. They are separated,
and must be, for any effective analysis of the contribution of the tail
to the aircraft stability and control.


What you wrote contradicted someone's claim. And that's all it
did. It's easy to contradict anyone.
Maybe you could provide some references that say that the
effectiveness of each piece can be calculated as a separate item,
disregarding the effects of the other, adjacent parts, and then
arriving at an accurate overall lift simply by summing them. We'd be
very interested to see such proof.

Dan

wrote in news:13c4f3ca-ac69-4672-a6a0-
:

On May 8, 4:44 pm, nospam wrote:

What I wrote totally contradicts your claim that the functions of the
components of an aircraft tail cannot be separated. They are
separated,
and must be, for any effective analysis of the contribution of the
tail
to the aircraft stability and control.


What you wrote contradicted someone's claim. And that's all it
did. It's easy to contradict anyone.
Maybe you could provide some references that say that the
effectiveness of each piece can be calculated as a separate item,
disregarding the effects of the other, adjacent parts, and then
arriving at an accurate overall lift simply by summing them. We'd be
very interested to see such proof.

I'd buy a lottery ticket and vote for Pat Paulson immediatly afterwards.


Bertie