Accession Number : AD0620677
Title : WEIGHT MINIMIZATION OF HONEYCOMB HEAT SHIELDS.
Descriptive Note : Final rept. for Mar-Apr 65,
Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Achard,Robert T.
Report Date : JUN 1965
Pagination or Media Count : 25
Abstract : A procedure for the design of minimum weight honeycomb structures for use as radiative heat shields is presented. Formulations are applicable to panels critical to intracell buckling and face compressive yield. Minimum weight is shown to occur at the condition where design variables produce a critical buckling stress equal to the compressive yield stress. (Author)
Descriptors : (*HEAT SHIELDS, HONEYCOMB CORES), WEIGHT, SANDWICH PANELS, BUCKLING, COMPRESSIVE PROPERTIES, STRESSES, MATHEMATICAL ANALYSIS, FAILURE(MECHANICS), PANELS, AEROSPACE CRAFT
Distribution Statement : APPROVED FOR PUBLIC RELEASE