Torsional Vibration of a Rotating Tapered-Twisted Turbomachine Blade Continental Aviation and Engineering Corporation

Format:

Conference/Event

Author/Creator:

Krupka, R. M., author.

Conference Name:

1970 Automotive Engineering Congress and Exposition (1970-01-12 : Detroit, Michigan, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1970

Summary:

This paper treats the torsional vibration of a rotating tapered and twisted turbomachine blade. Carnegie's formulation of the Lagrange equations of motion is used and the set of field equations solved using Myklestad's adaptation of the Holzer method. Digital computer results are presented for a particular turbine blade, demonstrating the convergence of the method and the satisfaction of the boundary conditions of the problem.The equations and methodology required to construct a digital computer program, in order to obtain a numerical solution to the problem, have been derived

Notes:

Vendor supplied data

Publisher Number:

700180

Access Restriction:

Restricted for use by site license