Vibratory Response of a Cylindrical Shell with Fixed Ends Subjected to a Unit Step Change of Pressure Northrop Corporation Electro-Mechanical Div

Format:

Conference/Event

Author/Creator:

Krupka, R. M., author.

Conference Name:

Aerospace Technology Conference & Exposition (1985-10-14 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1985

Summary:

The solution to the problem of establishing the value of the maximum stress in a uniform cylinder with fixed ends, subjected to a unit step change in pressure is presented. It is shown that the ratio of the maximum transient stress to the steady-state stress is a monotonically decreasing function of the damping ratio of the shell. The stress ratio approaches a value of 2 as the damping ratio and the parameter ψ, defined as

Notes:

Vendor supplied data

Publisher Number:

851984

Access Restriction:

Restricted for use by site license