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Isogrid structuresTest results and related structural instability analyses are presented for a 10-foot-diameter, 37-inch-long cylinder, and a 10-foot-diameter, 40-inch-long, 45-degree conical frustum. Both structures are based upon flanged isogrids and are fabricated in 2024-T851 aluminum. Peak edge load intensities at failure were 1,654 lb/in for the cylinder and 1,457 lb/in at the small diameter of the frustum. General instability cylindrical-monocoque-structure equivalent knockdown factors for both were in good agreement (gamma = 0.48). Design analysis is also derived for estimating critical cylinder instability edge loads from the performance of two tandem isogrid members. Evaluation is made of effective skin contributing to isogrid load-carrying cross-section.
Document ID
19750048628
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Slysh, P.
Dyer, J. E.
(General Dynamics Corp. Convair Div., San Diego, Calif., United States)
Furman, J. H.
Key, J. E.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 75-816
Meeting Information
Meeting: AIAA, ASME, and SAE, Structures, Structural Dynamics, and Materials Conference
Location: Denver, CO
Start Date: May 27, 1975
End Date: May 29, 1975
Sponsors: SAE, AIAA, ASME
Accession Number
75A32700
Funding Number(s)
CONTRACT_GRANT: NAS8-29859
Distribution Limits
Public
Copyright
Other

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