NDLI: Evaluation of a metal shear web selectively reinforced with filamentary composites for space shuttle application. phase 3 summary report: shear web component testing and analysis

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Evaluation of a metal shear web selectively reinforced with filamentary composites for space shuttle application. phase 3 summary report: shear web component testing and analysis

Content Provider	NASA Technical Reports Server (NTRS)
Author	Laakso, J. H. Straayer, J. W.
Copyright Year	1973
Description	Three large scale advanced composite shear web components were tested and analyzed to evaluate application of the design concept to a space shuttle orbiter thrust structure. The shear web design concept consisted of a titanium-clad + or - 45 deg boron/epoxy web laminate stiffened with vertical boron/epoxy reinforced aluminum stiffeners. The design concept was evaluated to be efficient and practical for the application that was studied. Because of the effects of buckling deflections, a requirement is identified for shear buckling resistant design to maximize the efficiency of highly-loaded advanced composite shear webs. An approximate analysis of prebuckling deflections is presented and computer-aided design results, which consider prebuckling deformations, indicate that the design concept offers a theoretical weight saving of 31 percent relative to all metal construction. Recommendations are made for design concept options and analytical methods that are appropriate for production hardware.
File Size	24134864
Page Count	243
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19730023044
Archival Resource Key	ark:/13960/t4zh1db0k
Language	English
Publisher Date	1973-08-01
Access Restriction	Open
Subject Keyword	Space Vehicles Component Reliability Structural Weight Composite Materials Webs Supports Epoxy Compounds Titanium Reinforced Plates Boron Compounds Space Shuttle Orbiters Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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