| dc.creator |
Johns, D. J. |
|
| dc.creator |
Houghton, D. S. |
|
| dc.creator |
Webber, J. P. H. |
|
| dc.date |
2014-12-04T09:40:34Z |
|
| dc.date |
2014-12-04T09:40:34Z |
|
| dc.date |
1961-05 |
|
| dc.date.accessioned |
2022-05-09T10:17:28Z |
|
| dc.date.available |
2022-05-09T10:17:28Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/8847 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4821 |
|
| dc.description |
Thermal stress distributions in uniform circular cylindrical shells due to axial
temperature distributions are investigated. The discontinuity effect due to the presence
of a cooler stiffening bulkhead is considered, and the possibility of thermal buckling of
the shell due to the circumferential discontinuity stress is examined. The buckling
analysis is based on Donnell's shell equation, and particular attention is given to shells
having clamped edges.
An experimental investigation of this buckling problem is discussed, and the results
obtained are seen to agree reasonably well with theory. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics |
|
| dc.relation |
College of Aeronautics Reports |
|
| dc.relation |
147 |
|
| dc.relation |
COA/147 |
|
| dc.title |
Buckling due to thermal stress of cylindrical shells subjected to axial temperature distributions |
|
| dc.type |
Report |
|