Stability of Very Flexible Aircraft with Coupled Nonlinear Aeroelasticity and Flight Dynamics
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Beijing Institute of Mechanical and Electrical Engineering, 100074 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034162
Reference36 articles.
1. Effect of multiple engine placement on aeroelastic trim and stability of flying wing aircraft
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