Flight Dynamics Issues of Control Coupling / Inertia Coupling Prone High-Speed Aircraft
Document Type
Conference Proceeding
Publication Date
7-29-2024
Abstract
Excerpt: The authors developed a nonlinear, time-domain aircraft flight simulation program to determine the transient, open-loop response of the Bell X-1A Aircraft. With this tool, we demonstrated the response of the X-1A to aileron inputs at select points in its flight envelope.
Source Publication
AIAA AVIATION FORUM AND ASCEND 2024
Recommended Citation
Quintero, E. U., Takahashi, T. T., & Grandhi, R. (2024). Flight Dynamics Issues of Control Coupling / Inertia Coupling Prone High-Speed Aircraft. AIAA AVIATION FORUM AND ASCEND 2024, Session: Flight Dynamics Issues in Aircraft Design, AIAA 2024-4048. https://doi.org/10.2514/6.2024-4048
Comments
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
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