NASA NTRS · 19900000865
Composite Blade Structural Analyzer (COBSTRAN) theoretical/programmer's manual
Abstract
This manual describes the organization and flow of data and analysis in the computer code, COBSTRAN (COmposite Blade STRuctural ANalyzer). This code combines composite mechanics and laminate theory with an internal data base of fiber and matrix properties and was developed for the design and analysis of composite turbofan and turboprop blades and composite wind turbine blades. Inputs to the code are constituent fiber and matrix material properties, factors reflecting the fabrication process, composite geometry and blade geometry. COBSTRAN performs the micromechanics and laminate analyses of these fiber composites and generates a NASTRAN finite element model of the blade. This manual describes the equations formulated and solved in the code and the function of each of the seventy-two subroutines. COBSTRAN is written in FORTRAN 77.
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Aiello, Robert A., Chamis, Christos C.. 1989-08-01. Composite Blade Structural Analyzer (COBSTRAN) theoretical/programmer's manual. https://ntrs.nasa.gov/citations/19900000865
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