Accession Number:

ADA003083

Title:

The Stability of Shells during Thermal Shock,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-11-19

Pagination or Media Count:

11.0

Abstract:

The stability of a smooth circular cylindrical shell is examined, to whose face heat flux is suddenly supplied. The lateral surface of the shell is ideally heat-insulated. It is assumed that the thermoelastic waves, which are propagated along the generatrix, are compression waves and with the value of the heat flux exceeding its critical value, can cause oscillatory instability of the shell.

Subject Categories:

  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE