Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method

This work presents the development of closed-form expressions for the aerodynamic stability derivatives of wings and aircraft flying at subsonic compressible conditions using the unsteady subsonic 3D source and doublet panel method (SDPM). The stability derivatives are obtained directly from the fre...

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Veröffentlicht in:	Journal of aircraft 2024-07, Vol.61 (4), p.1034-1046
Hauptverfasser:	Dimitriadis, Grigorios, Panagiotou, Pericles, Dimopoulos, Thomas, Yakinthos, Kyros
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic stability Aerodynamics Aerospace & aeronautics engineering Aircraft Aircraft configurations Angle of attack Blended-Wing-Body aircraft Compressibility Computational efficiency Computational fluid dynamics Computing costs Engineering, computing & technology Flight Dynamics Ingénierie aérospatiale Ingénierie, informatique & technologie Mathematical analysis Methodology Military aircraft Panel method (fluid dynamics) Panel methods Sideslip Stability derivatives Subsonic aircraft Swept wings Unmanned aerial vehicles Unmanned aircraft Wind tunnel testing Wind tunnels Wings (aircraft) Yaw
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