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

Technology

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 divergence, control reversal, flutter, trajectory perturbations, structural strains and stresses, structural load resultants, etc.

Ready to Sign License Available

Please visit our Ready to Sign instructions page to learn how to request a license. The two types of licenses available for ASWING and their respective costs include the following (please click on either type below to download the license as a fillable PDF): 

Contact the TLO to request a Government Contractor or Agency license.

Questions? Contact software-licenses@mit.edu.