TEMPERATURES AND THERMAL STRESSES IN THIN-WALLED SPHERICAL SEGMENTS.
Abstract
The thermal stresses induced in thin-walled spherical shell seqments, subject to a uniform aerodynamic heat input are presented. The problem is divided into two main sections: determination of the transient and steady-state temperature distribution in the spherical shell segment, and calculation of the resulting thermal stresses. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1969
- Accession Number
- AD0688433
Entities
People
- Brice N. Cassenti
- S. V. Nardo
Organizations
- New York University Tandon School of Engineering