NASA NTRS · 19810000245
Composite-Material Point-Stress Analysis
Abstract
PSANAL computes composite-laminate elastic and thermal properties and allowable load levels for any combination of applied membrane and bending loads occurring at a point. Basic linear orthotropic stress/ strain relationships and standard composite-laminate theory formulas are utilized.
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Spears, F., S.. 1982-11-01. Composite-Material Point-Stress Analysis. https://ntrs.nasa.gov/citations/19810000245
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