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A new technique for simulating composite materialThis project dealt with the development on new methodologies and algorithms for the multi-spectrum electromagnetic characterization of large scale nonmetallic airborne vehicles and structures. A robust, low memory, and accurate methodology was developed which is particularly suited for modern machine architectures. This is a hybrid finite element method that combines two well known numerical solution approaches. That of the finite element method for modeling volumes and the boundary integral method which yields exact boundary conditions for terminating the finite element mesh. In addition, a variety of high frequency results were generated (such as diffraction coefficients for impedance surfaces and material layers) and a class of boundary conditions were developed which hold promise for more efficient simulations. During the course of this project, nearly 25 detailed research reports were generated along with an equal number of journal papers. The reports, papers, and journal articles are listed in the appendices along with their abstracts.
Document ID
19920001922
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Volakis, John L.
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:188792
UMICH-025921-23-T
NASA-CR-188792
Report Number: NAS 1.26:188792
Report Number: UMICH-025921-23-T
Report Number: NASA-CR-188792
Accession Number
92N11140
Funding Number(s)
CONTRACT_GRANT: NAG2-541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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