Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A
Author:
Affiliation:
1. NASA Dryden Flight Research Center
2. NASA Kennedy Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6312
Reference5 articles.
1. Development and Testing of Control Laws for the Active Aeroelastic Wing Program
2. 3Murray,J.E.,andMaine,R.E."pEstVersion2.1User'sManual,"NASATechnicalMemorandum88280,1987.
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