Thermal Stresses in Disks of Constant Thickness
Abstract
TURBINE disks are subject to stresses due to two causes; the inertia effects of rotation, and the radial variation of temperature across the disk. Elastic stresses due to each of these effects may be determined separately and superposed to obtain the resultant stress distribution.
Citation
Norbury, J.F. (1957), "Thermal Stresses in Disks of Constant Thickness", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 5, pp. 132-137. https://doi.org/10.1108/eb032823
Publisher
:MCB UP Ltd
Copyright © 1957, MCB UP Limited