Hi community,
currently I am doing some structural analysis with loads resulting from required Limit manoeuvring load factor.
In CS VLR.337 following requirement is listed:
The rotorcraft must be designed for-
(a) A limit manoeuvring load factor ranging from a
positive limit of 3.5 to a...
Hi @ all,
I'm a stress eng. with approx. 1 year experience but only on fixed wing AC. Since I have a new job, where we produce some rotorcraft UAV's, I have to do stress calculations of each part of the rotorcraft. Unfortunately I couldn't find any literature dealing with the topics of stress...
Hi,
I'm currently trying to solve the problem, attached to the pdf-file. It's a hyperstatic system due to the fact that it's connected by two solid bearings (2 DOF*2). The forces in the horizontal direction, H1 and H7, are calculated but the vertical forces are kind of replaced? by K. Force F2...
