Accession Number:

AD0432024

Title:

THERMAL STRESS DETERMINATION TECHNIQUES FOR SUPERSONIC TRANSPORT AIRCRAFT STRUCTURES

Descriptive Note:

Corporate Author:

BELL AEROSYSTEMS CO BUFFALO NY

Report Date:

1964-01-01

Pagination or Media Count:

128.0

Abstract:

This report describes computer programs developed for the analysis of heated beams, plates, and stiffened cylindrical shells. The matrix displacement approach to structural analysis, which forms the theoretical basis of these programs, is developed in detail. Derivation of new relationships employed in these programs is also detailed. The capabilities and limitations of the respective programs are outlined and illustrative applications are presented.

Subject Categories:

  • Civilian Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE