Accession Number : AD0432024


Title :   THERMAL STRESS DETERMINATION TECHNIQUES FOR SUPERSONIC TRANSPORT AIRCRAFT STRUCTURES


Corporate Author : BELL AEROSYSTEMS CO BUFFALO NY


Personal Author(s) : Gallagher, R H ; Padlog, J ; Huff, R D


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/432024.pdf


Report Date : Jan 1964


Pagination or Media Count : 128


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.


Descriptors :   *SUPERSONIC AIRCRAFT , DATA PROCESSING , DEFLECTION , ELASTIC PROPERTIES , MEASUREMENT , STRUCTURES , THERMAL STRESSES


Subject Categories : Civilian Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE