An Integrated Low-Speed Aeroelastic-Flight-Dynamics Framework for Modeling Supersonic Aircraft
Author:
Affiliation:
1. University of Michigan
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2175
Reference21 articles.
1. Introduction to the Special Section on the Prediction of F-16XL In-Flight Aerodynamics
2. Toward Improved Predictions of Slender Airframe Aerodynamics Using the F-16XL Aircraft
3. F-16XL Simulations at Flight Conditions Using Hybrid Near-Body/Offbody Computational Fluid Dynamics
4. Numerical Simulations of the F-16XL at Flight-Test Conditions Using Delayed Detached-Eddy Simulation
5. Computational Fluid Dynamics Predictions of Control-Surface Effects for F-16XL Aircraft
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