ASWING Software for Aerodynamic, Structural, and Control-response Analysis of Aircraft

Technology #7821

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ASWING software
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Inventors
Professor Mark Drela
Department of Aeronautics & Astronautics, MIT
External Link (aeroastro.mit.edu)
Managed By
Daniel Dardani
MIT Technology Licensing Officer

ASWING is a software program for the aerodynamic, structural, and control-response analysis of aircraft with flexible wings and fuselages of high to moderate aspect ration.  Static, time-domain dynamic, and frequency-domain dynamic analyses can be performed, allowing predictions of diverence, control reversal, flutter, trajectory pertubations, structural strains and stresses, structural load resultants, etc.

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