Method presented for determination of contour of disks, typified by those of aircraft gas turbines, to incorporate arbitrary elastic stress distributions resulting from either centrifugal or combined centrifugal and thermal effects. (15¢)
Direct method of design and stress analysis of rotating disks with temperature gradient
Nat Advisory Committee Aeronautics -- Report
1950
14 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Direct method of design and stress analysis of rotating disks with temperature gradient
Engineering Index Backfile | 1949
|Methods of stress calculation in rotating disks
TIBKAT | 1944
|Numerical Analysis of a Rotating Cylinder with Spanwise Disks
Online Contents | 2012
|