Frequency Domain Method for Dynamic Control Derivative Estimation with Application to Transonic Truss-Braced Wing

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Veröffentlicht in:AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 4 of 5
1. Verfasser: Nguyen, Nhan T. (VerfasserIn)
Weitere Verfasser: Xiong, Juntao (VerfasserIn)
Pages:4
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2023
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