Detached Eddy Simulation for the F-16XL Aircraft Configuration
Author:
Affiliation:
1. NASA Langley Research Center
2. ViGYAN, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1496
Reference21 articles.
1. Overview of the Cranked-Arrow Wing Aerodynamics Project International
2. Comparison of Measured and Block Structured Simulation Results for the F-16XL Aircraft
3. Standard Unstructured Grid Solutions for Cranked Arrow Wing Aerodynamics Project International F-16XL
4. Lessons Learned from Numerical Simulations of the F-16XL Aircraft at Flight Conditions
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1. An Improved Nonlinear Aerodynamic Derivative Model of Aircraft at High Angles of Attack;International Journal of Aerospace Engineering;2021-09-08
2. Synthesis of Hybrid Computational Fluid Dynamics Results for F-16XL Aircraft Aerodynamics;Journal of Aircraft;2017-11
3. F-16XL Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulation on Unstructured Grids;Journal of Aircraft;2017-11
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