... which show how (A) the rudder/aileron/elevator is constructed externally and internally, and how exactly that component is attached to the aircraft, would be of help. This is for a project we're working on. While, apparently, the office in question has gotten approval to send us diagrams for the actual aircraft of interest, the PAPERWORK hasn't gotten done, and time is getting short.
I've been doing some online searches but either my Google-fu is WEAK!!! or nothing is out there. Right now I'd take anything from a reasonably modern jet aircraft, preferably a fighter or something like it, but I'll settle even for a commercial jet.
The project is for monitoring key stress points on these control surfaces, so what I'm most interested in are the attachment points and other areas which will be bearing the stress when the surface is in use.
I've been doing some online searches but either my Google-fu is WEAK!!! or nothing is out there. Right now I'd take anything from a reasonably modern jet aircraft, preferably a fighter or something like it, but I'll settle even for a commercial jet.
The project is for monitoring key stress points on these control surfaces, so what I'm most interested in are the attachment points and other areas which will be bearing the stress when the surface is in use.
no subject
Date: 2009-08-10 01:05 pm (UTC)no subject
Date: 2009-08-10 01:16 pm (UTC)no subject
Date: 2009-08-10 06:32 pm (UTC)Also, unless you are dealing with bleeding edge jets, remember they've usually been around for a while. The F-15 design was approved in 1969, the F/A-18 and the Super Hornet are derived from a design dated early 1965, the first prototype that led to the F-117 flew in 1975, and so on.
no subject
Date: 2009-08-10 08:40 pm (UTC)http://www.box.net/shared/sgl0tbglxl
no subject
Date: 2009-08-10 10:22 pm (UTC)http://pics.livejournal.com/laptop_mechanic/pic/002560xk
no subject
Date: 2009-08-11 02:58 am (UTC)no subject
Date: 2009-08-11 11:05 am (UTC)http://pics.livejournal.com/laptop_mechanic/gallery/0003bxdz
no subject
Date: 2009-08-11 02:39 pm (UTC)I certainly accept the possibility I'm blind.
no subject
Date: 2009-08-11 02:57 pm (UTC)no subject
Date: 2009-08-12 01:00 am (UTC)http://www.flickr.com/photos/taiaselene/sets/72157615126828102/
no subject
Date: 2009-08-13 12:45 pm (UTC)Of possible help...
Date: 2009-08-13 04:39 am (UTC)Should get you to the Google Images page with lots of control surface pictures. The search words were "aircraft control surfaces".
A bit of background material at: http://en.wikipedia.org/wiki/Aircraft_flight_control_systems
A little bit about structural design at:
http://adg.stanford.edu/aa241/structures/structuraldesign.html
Is this for a literary project (iceberg time) or is it an engineering project?
Re: Of possible help...
Date: 2009-08-13 12:51 pm (UTC)What I'm trying to find out is how (for example) the rudder, elevators, and/or ailerons are constructed internally, and specifically how they are fastened to the aircraft and controlled.
From what I can see, they're attached by two or more points to a bar of metal that's the rotating part of a hinge -- basically, they're like a little door, and the attachment points are the places where the hinges attach. What I don't know is how they're constructed internally, whether that's empty air or foam or what inside, etc., and whether they're generally covered by something when in use. Also whether they're closed metal boxes with just the attachment points to the bar sticking out, or not.