Skip Top nav bar link group topnav end piece go to business section go to education section go to history section go to gallery section go to news section go to organizations section go to research section go to search engine go to site index topnav end piece
NASA Meatball Banner of Dryden Flight Research Center
white space
Image of gray corner
Dryden Technical Reports Server banner with text and picture of a book
[Home] [About] [Browse] [Search] [User Area] [Help]

Elastic Constants for Superplastically Formed/Diffusion-Bonded Corrugated Sandwich Core

Ko, William L. (1980) Elastic Constants for Superplastically Formed/Diffusion-Bonded Corrugated Sandwich Core. Technical Report NASA TP-1562, Research Engineering, NASA Dryden Flight Research Center.

Full text available as:
PDF - Requires Adobe Acrobat Reader or other PDF viewer.

Abstract

This paper presents formulae and associated graphs for evaluating the effective elastic constants for a superplastically formed/diffusion-bonded (SPF/DB) corrugated sandwich core. The results were used in the comparison of structural stiffnesses of the above sandwich core and a honeycomb core under conditions of equal sandwich core density. It was found that the stiffness in the thickness direction of the optimum SPF/DB corrugated core (that is, triangular truss core) was lower than that of the honeycomb core, and that the former had higher transverse shear stiffness than the latter.

EPrint Type:NASA Technical Publication
Keywords:Stiffness, Structural properties
Subjects:Aircraft/Project: Nonaircraft-specific
(31 - 39) Engineering: (39) Structural Mechanics
ID Code:644
Deposited On:09 Febuary 2006
Additional Information:82 pages. This report is an expanded version of "Elastic Constants for Superplastically Formed/Diffusion-Bonded Sandwich Structures" by the same author (AIAA Paper No. 79-0756).
blank space image of gray corner

 

Last Modified: September 14, 2004
Responsible NASA Official: Jenny Baer-Riedhart
Webmasters

NASA Web Privacy Statement