On the design of a row of windows in a pressurized cylindrical fuselage

dc.contributor.author	E. H. Mansfield	en_US
dc.date.accessioned	2014-10-21T15:55:59Z
dc.date.available	2014-10-21T15:55:59Z
dc.date.issued	1963	en_US
dc.identifier.other	ARC/R&M-3360	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3942
dc.description.abstract	Some factors affecting the design of a row of windows in a pressurized cylindrical fuselage are discussed. The concept of the neutral hole is adopted, but account is taken of the change in the basic 2:1 stress field occasioned by the presence of stringers, frames, longerons and, in particular, reinforced strips surrounding the windows and running the length of the fuselage. The influence of such reinforcement is to make the shape of the neutral hole slightly more circular than the standard √/2:1 ellipse. Results are presented in graphical form.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	On the design of a row of windows in a pressurized cylindrical fuselage	en_US