The leading-edge buckling of a thin built-up wing due to aerodynamic heating

dc.contributor.author	K. I. McKenzie	en_US
dc.date.accessioned	2014-10-21T15:55:46Z
dc.date.available	2014-10-21T15:55:46Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3295	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3873
dc.description.abstract	An analysis is presented of the buckling of the leading edge of a thin built-up wing subjected to spanwise thermal stress. Computed values of the buckling load are given in graphical form for a wide variation of leading-edge dimensions and these results are used to obtain buckling criteria for some specific examples.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The leading-edge buckling of a thin built-up wing due to aerodynamic heating	en_US