Thermal stresses in thin cylindrical shells, stiffened by plane bulkheads, for arbitrary temperature distributions

Johns, D. J.

dc.contributor.author	Johns, D. J.
dc.date.accessioned	2017-04-26T15:24:58Z
dc.date.available	2017-04-26T15:24:58Z
dc.date.issued	1958-07
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/11828
dc.description.abstract	A study has been made of the thermal stresses reulting near the joint of a cylinder and internal bulkhead due to arbitrary temperature distributions in the configuration and to the consequent compatability forces and moments at the joint. The method is general enough to permit the inclusion of joint thermal resistance but certain limitations are placed on the form of the axial temperature distribution in the cylinder. An approximate method to determine the transient temperatures for completely general heating programmes is also proposed.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics	en_UK
dc.relation.ispartofseries	CoA/N-83	en_UK
dc.relation.ispartofseries	83	en_UK
dc.title	Thermal stresses in thin cylindrical shells, stiffened by plane bulkheads, for arbitrary temperature distributions	en_UK
dc.type	Report	en_UK