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Advanced composites structural concepts and materials technologies for primary aircraft structures. Structural response and failure analysis: ISPAN modules users manualThe ISPAN Program (Interactive Stiffened Panel Analysis) is an interactive design tool that is intended to provide a means of performing simple and self contained preliminary analysis of aircraft primary structures made of composite materials. The program combines a series of modules with the finite element code DIAL as its backbone. Four ISPAN Modules were developed and are documented. These include: (1) flat stiffened panel; (2) curved stiffened panel; (3) flat tubular panel; and (4) curved geodesic panel. Users are instructed to input geometric and material properties, load information and types of analysis (linear, bifurcation buckling, or post-buckling) interactively. The program utilizing this information will generate finite element mesh and perform analysis. The output in the form of summary tables of stress or margins of safety, contour plots of loads or stress, and deflected shape plots may be generalized and used to evaluate specific design.
Document ID
19950003830
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hairr, John W.
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Huang, Jui-Ten
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Ingram, J. Edward
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Shah, Bharat M.
(Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-4449
LG92ER0036
NAS 1.26:4449
Report Number: NASA-CR-4449
Report Number: LG92ER0036
Report Number: NAS 1.26:4449
Accession Number
95N10242
Funding Number(s)
PROJECT: RTOP 510-02-13-01
CONTRACT_GRANT: NAS1-18888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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