Mr.RSrandazzo
I do not really feel the need to mix my professional work life, and my hobby together. But since some users are unable to understand how thermodynamics works, I think it would be potentially valuable for the community if I offer my skills. I am a Mechanical Engineering who mostly looks at strengths of materials, but I have had to do a fair amount work on the life cycles of parts under thermodynamic loads. What I would like to do is a Computational Fluid Dynamic study of for the R-2800’s. In order to see what the equation the values should be based on the values that are used in the sim, vs the real numbers vs the CFD study. I know that we see very little if any difference between three. There is no one can argue with the numbers, so I think this will put a stop to the engine debate that people are having. I thought I once read claims of someone comparing your DC3 engines [i assume R-1830’s] to the engines in your simulated DC6. If this is the case, then I would like to try and get a CFD done on those to map the relative thermal similarity of the engine (at their hottest running conditions).
I would not feel comfortable commenting on what I believe is happening or the misconception these people are “seeing” without being able to run the numbers through a couple different scenarios (prop-wash cowls closed, tail wind cowls closed with max/min prop wash).
I only really fly x-plane so being part of Avsim community was not really a needed thing until I took a look at the forum to see what people were saying, and I could not believe it.
I look forward to talking more in specific details, and working out a way to get this information to the masses.
Look Forward to Talking more,
Nick Paine
P.S. I cannot change the signature until 14 June. So that is why I signed here.