High-Angle-of-Attack F-16XL Flight Simulations at Sub- and Transonic Speeds
Author:
Affiliation:
1. Airbus Defence and Space, 83064 Manching, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034025
Reference33 articles.
1. Applying slender wing benefits to military aircraft
2. ChambersJ. R. “High Angle of Attack Aerodynamics: Lessons Learned,” AIAA Paper 1986-1778 CP, 1986.
3. Some vortical-flow flight experiments on slender aircraft that impacted the advancement of aeronautics
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