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Search: Posts Made By: TURIN
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Forum: Tech Log
24th Feb 2018, 09:27
Replies: 95
Views: 32,257
Posted By TURIN

Not necessarily. The tailplane just needs to be...

Not necessarily. The tailplane just needs to be producing less downforce than needed.
Forum: Tech Log
25th May 2012, 22:26
Replies: 95
Views: 32,257
Posted By TURIN

Like I said. Life's too short to get into...

Like I said. Life's too short to get into pointless discussion such as this. I enter into pprune to learn and hopefully pass on some of my experience that others may also learn. If you want to get...
Forum: Tech Log
25th May 2012, 19:04
Replies: 95
Views: 32,257
Posted By TURIN

Oh dear! Italia 458, As I'm not from North...

Oh dear! Italia 458, As I'm not from North America I can't say either way if your rant is accurate our not.
However, one thing is certain. You need to settle down. My quoted post was meant to be...
Forum: Tech Log
20th May 2012, 09:44
Replies: 95
Views: 32,257
Posted By TURIN

Not much to be doing with failure modes either -...

Not much to be doing with failure modes either - if the CG is ahead of the aerodynamic centre the aircraft will be statically stable whatever the FBW is doing.

[/QUOTE]

I think we are in...
Forum: Tech Log
19th May 2012, 11:19
Replies: 95
Views: 32,257
Posted By TURIN

My understanding of tail (trim tank) fuel is to...

My understanding of tail (trim tank) fuel is to reduce the amount of trim and therefore drag, not to swap pitch up trim for pitch down trim. The a/c still needs to be stable. Especially air...
Forum: Tech Log
18th May 2012, 21:57
Replies: 95
Views: 32,257
Posted By TURIN

To answer your last point. Yes, but the a/c would...

To answer your last point. Yes, but the a/c would not be naturally stable.
Forum: Tech Log
16th May 2012, 15:20
Replies: 95
Views: 32,257
Posted By TURIN

"Most people find mathematics a very useful...

"Most people find mathematics a very useful common language in these circumstances. It introduces a discipline that avoids the sort of confusion etc etc. "

I have to disagree. Most people use the...
Forum: Tech Log
15th May 2012, 21:52
Replies: 95
Views: 32,257
Posted By TURIN

No I wouldn't. AofA (I thought) is the...

No I wouldn't.

AofA (I thought) is the angle between chord line and relative airflow.

If the angle between chord and airflow reduces then AofA reduces and vice-versa.

If the angle reduces...
Forum: Tech Log
15th May 2012, 18:30
Replies: 95
Views: 32,257
Posted By TURIN

I do not understand how this statement can be...

I do not understand how this statement can be true of a 'conventional', stable, aircraft design.


Please indulge me for a moment while I work this through as I know from previous experience that...
Showing results 1 to 9 of 9


 
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