CFD Based Model Building of the F-16XL Static and Dynamic Loads Using Kestrel
Author:
Affiliation:
1. CREATE Kestrel Team
2. University of Alabama, Birmingham
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0286
Reference26 articles.
1. Towards an Efficient Aircraft Stability and Control Analysis Capability Using High-Fidelity CFD
2. Aircraft Stability and Control Characteristics Determined by System Identification of CFD Simulations
3. Determining the Applicability and Effectiveness of Current CFD Methods in Store Certification Activities
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