Asymmetrical Bending of Tapered Disks: The Solution of a Problem in Disk Bending Occurring in Connexion with Gas Turbines

Abstract

THE problem considered is that of a tapered bored disk, built‐in at the inner edge and twisted about a diameter, the outer edge remaining plane and circular. The outer edge may be regarded as:

Citation

Gradwell, C.F. (1950), "Asymmetrical Bending of Tapered Disks: The Solution of a Problem in Disk Bending Occurring in Connexion with Gas Turbines", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 7, pp. 209-212. https://doi.org/10.1108/eb031926