Geometry driven high fidelity stability derivatives using an automated CFD analysis process

Publication source: 
16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Publication authors: 
Bhagat N., Allison D. L., Alyanak E.
Scope of application: 
Aerospace
Organizations of authors: 
Wright State Research Institute, Optimal Flight Sciences LLC, Air Force Research Laboratory
Country: 
US
Year of publication: 
2015