Axisymmetric mode of deformation of cylinders subjected to compressive end loads is examined with aid of available theory; stresses and deformations obtained with theory are compared with those of 7075-T6 Al-alloy cylinder with high internal pressure; behavior of cylinder was in agreement with predictions; pertinence to aircraft fuselage and missiles.
Structural behavior of pressurized, ring-stiffened, thin-wall cylinders subjected to axial compression
NASA -- Tech Note
1960
24 pages
Report
English
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Bending and compression tests of pressurized ring-stiffened cylinders
Engineering Index Backfile | 1960
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