10.2514/6.2024-4048">
 

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.

Comments

© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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Source Publication

AIAA AVIATION FORUM AND ASCEND 2024

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