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A new method is presented for the fast calculation of the time-varying aerodynamic loads acting on aircraft flying at high subsonic airspeeds. It is shown that the approach can match experimental data from wind tunnel testing.
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This page is a summary of: Transonic Corrections for the Unsteady Compressible Source and Doublet Panel Method, Journal of Aircraft, May 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c038024.
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