NASA NTRS · 19750011101
Improvements to the SADSAM computer program for aeroelasticity analysis
Abstract
A computer program for calculating the elastic element forces and strain energy distribution for normal mode shapes is presented. The subjects discussed are: (1) revised aerodynamic force representation, (2) flap aerodynamics, (3) chordwise motions and aerodynamic forces, (4) wing-tail interaction, and (5) gust analysis. An aircraft configuration used in sample gust analysis is included.
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Schwendler, R. G.. 1975-03-01. Improvements to the SADSAM computer program for aeroelasticity analysis. https://ntrs.nasa.gov/citations/19750011101
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