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CFD-Based Frequency Domain Method for Dynamic Control Derivative Estimation with Application to Transonic Truss-Braced Wing
Document ID
20230008558
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nhan Nguyen (Ames Research Center Mountain View, California, United States)
Juntao Xiong (Wyle (United States) El Segundo, California, United States)
Date Acquired
June 2, 2023
Subject Category
Aircraft Stability and Control
Meeting Information
Meeting: AIAA Aviation Forum
Location: San Diego, CA
Country: US
Start Date: June 12, 2023
End Date: June 16, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.01.15.01.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Aircraft Control Derivative

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