Article navigation

THE matrix flexibility method for the prediction of the normal modes of vibration of a structure may be extended to the case of a structure which has no external supports. This is of particular relevance to problems of aircraft and missile vibration.

This content is only available via PDF.
You do not currently have access to this content.
Don't already have an account? Register

Purchased this content as a guest? Enter your email address to restore access.

Pay-Per-View Access
$39.00
Rental

or Create an Account

Close Modal
Close Modal