NASA NTRS · 20230008558
CFD-Based Frequency Domain Method for Dynamic Control Derivative Estimation with Application to Transonic Truss-Braced Wing
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Nhan Nguyen, Juntao Xiong. CFD-Based Frequency Domain Method for Dynamic Control Derivative Estimation with Application to Transonic Truss-Braced Wing. https://ntrs.nasa.gov/citations/20230008558
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