No company will be willing to give this information for free even for educational purposes, that's why i thought I'll look around for some info before even trying to contact anyone.
I know that this is not easy, as i said I have a large group of people working and we have a lot of free time so...
and just to be clear, my analysis will be on the (turbine , intake , compressor , nozzle) so there aren't many parts to be drawn here.
i just need the aerothermal specifications and a blueprint for the shaft , blades, intake and propelling nozzle.
well I'm working with a group of 10 people so even if it was a scan copy we can digitize it that's not an issue .
here is an example of what I'm looking for http://www.dtic.mil/dtic/tr/fulltext/u2/804527.pdf
i would've used the one i linked but the copy is not clear and barley readable. no to...
Hello,
I'm doing a full stress analysis on a complete aircraft engine. so i was looking for documents with full specifications of the engine ( blueprints,charts,data tables, ...etc. ) .
I know that most of these information are top secret whether it's a civil engine a military engine.
However...
Sorry should have specified that I'm talking about rotor blades .
well that's the thing i couldn't find any paper or source that specifies the aerodynamic forces , i know they are very small compared to other stresses but my question is by how much and is it worth it to look into them.
I'm doing a survey on the topic of "gas turbine blades stress analysis" to see what areas are not focused on in this subject.
I've found that not many people talk about the aerodynamic forces on the blade. Am I missing something, are they included in the calculation or are they too small to...