LoL, get over yourself Bill! You're clueless on this subject and many others as you have so thuroughly demonstrated many times now. (Let me guess now Bill is going to pull up the suction debate, get ready to be sidetracked thread!)
And now Bill is trying suggest that I claimed bombers were designed for higher stress levels in terms of G forces!

This gets crazier by the post!
But hey, lets give Bill a chance to find that exact phrase where I according to him said: B-17's can make 12G turns, a P-51 can only take 8G, oh yes..
What you said was this
" Comparing fighters and bombers is pure nonesense. A bomber is far more ruggedly built and features much larger fuselage and wing sections
How much bigger is a Ju 88 (bomber version) compared to a Lightning or P-47? How much bigger is an A-20 or Douglas B-26 to an F-4 or F-105 or an A-10? Want to compare ruggedness or 'strength' in terms of ultimate or Limit loads?Do you want to compare the load capability and stress level capability of the 'bigger B-17' to the F-105? The B-17 is 8 feet longer - it must be stronger, right?
You live in the world of absolutes. Show us that 'bombers are built more ruggedly and are bigger'
Bill apparently doesn't know that the weight an a/c's wings have to carry is multiplied by the amount of G's excerted on the a/c.
I believe I do Soren. Illustrate that your 'bomber' is bigger and more ruggedly built and compare the load of a B-17, the speed, the G forces and the stresses that a B-17 can take versus an F-105?
I didn't claim that a 51 can take the total damage that a B-17. What I did say is that it is possible for a 51 to take a 30mm hit and survive. You said 'no way' and I asked you to prove it.. and here we are.
Soren - 'weak' and 'strong' are relative terms. Design Limit Loads and Ultimate Limit loads expressed in G forces are not. They are THE foundation for airframe design - not absolute forces. Any pilot and/or airframe guy would know that. Curiously, like aerodynamics, you are not familiar with the terminolgy or the context of terms that you use for airframe structures discussions.
Having a degree in engineering and practicing airframe structures in aviation industry is not relative except in contrast to your background.
I posted my degree Soren and invited you to post your credentials for your statements. I am still waiting.
What Bill also obviously doesn't know (Yep, he obviously really doesn't) is that bombers were DESIGNED BUILT to carry huge loads and at the same time to withstand enemy attacks!
Some bombers were designed better than others with respect to taking battle damage.. has nothing to do per se to Design Limit and Design Ultimate loads Soren.. Some bobers are much bigger than others, some bombers are smaller than fighters.
A B-17 empty cannot survive the stresses imposed by an 8g pullout that a 109 or Spit loaded can easily survive. An A-20 and Mossie are the closest 'bombers' to large fighter sizes can not take either the raw aerodynamic forces or the resultant stresses of an F4U or P-38 or P-47 even though the A-20 is 'bigger and heavier' and has a larger cross section and wingspan.
But just like I predicted Bill is now trying to suggest that a P-51 can take a direct hit from an 88mm!! Well yes, sure Bill ofcourse it can, it's a P-51 so it can ofcourse take more punishment than a bomber!

I mean if it takes the massive power of a single rifle round to down a P-51 I'm sure a cannon shell would be useless
You have both a severe reading and comprehension problem Soren. I have not said that..
Talk about sticking your nose into unknown territory!