Accession Number:

AD0657843

Title:

CREEP OF CONICAL MEMBRANE SHELLS UNDER AERODYNAMIC HEATING AND LOADING,

Descriptive Note:

Corporate Author:

STATE UNIV OF NEW YORK BUFFALO DIV OF INTERDISCIPLINARY STUDIES AND RESEARCH

Personal Author(s):

Report Date:

1967-07-01

Pagination or Media Count:

43.0

Abstract:

Expressions for the creep stresses and displacements in a conical shell at a small angle of attack to a supersonic flow field are obtained. The flow is assumed to be steady adiabatic and the cone is approximated by a membrane shell. Surface shear stresses are found to have a negligible effect on the solutions. On the other hand, temperature distributions which differ slightly from a given uniform valve result in displacements which differ significantly from those obtained using the uniform temperature. Author

Subject Categories:

  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE