The aim is for the frame to be mechanically fastened to the skin of the aircraft and in the case of scenario 1 the L frame (Cleat) will be fastened to the C Frame. As for the abuse of the aircraft, it will serve as a commercial aircraft similar in size, payload and operational conditions to a...
The Frame is there to support the entire fuselage skin. Whilst there are locations whereby floor beams and struts will be connected, the focus is mainly on a general approach in the acreage area. The indicated topics (Cost, Ease of manufacture and strength) are of course the main focus in the...
Hi, I'm trying to look into the benefits and disadvantages of different types of frame configurations for an aircraft fuselage assignment. The three options I have at the moment
1) is a mechanically fastened C+L Frames,
2)a Z Frame with some local pad ups on the web and
3)a one piece C+L...
Hi, I'm trying to look into the benefits and disadvantages of different types of frame configurations for an aircraft fuselage assignment. The three options I have at the moment
1) is a mechanically fastened C+L Frames,
2)a Z Frame with some local pad ups on the web and
3)a one piece C+L...
