Patch 4.10 - Development Updates by Daidalos Team

[MD_Titus]

more knowledge than the aircraft engineers that made these things?

[AndyJWest]

Ernst, I can see no point in even attempting to correct your misunderstanding of what is under discussion here. If you want to contribute anything useful, I suggest you study a little about the subject first, rather than making ridiculous claims based on balsa-wood and the carbon content of aluminium alloys.

As far as I'm concerned, unless somone can come up with meaningful comparative G-load figures, the topic is closed.

[Friendly_flyer]

I really, really like the personal plane lists idea! I really only fly a small subset of planes, and most of them are far down the list (i.e. Hurricane Mk.I). This is going to make my life a lot simpler!

[AndyJWest]

Originally Posted by Ernst

Would like to see this comparative g-loads figures too. Its difficult to find, if you known please post. Take a look here:

http://faa-engineers.com/~mjgundry/b...alculation.pdf

What do you say about? Can this procedure give us a clue?

http://www.flightsimaviation.com/dat...t_23-appA.html

http://faa-engineers.com/~mjgundry/b...alculation.pdf
"V Speed Determination for RW-11" The RW-11 seems to be an "Easy to build replica of the [Piper] Vagabond." What has this got to do with anything? No mention of G limits anyway.

http://www.flightsimaviation.com/dat...t_23-appA.html
Modern FAA regulations for a particular class of light aircraft - no mention of materials used - irrelevant to the topic under discussion.

Posting random off-topic articles is no way to settle anything. I'm going to ignore any further comments/links from you, unless someone else thinks they are worth considering.

[MD_Titus]

doubtful. i know near bugger all about that kind of stuff, and his posts read like nonsense.