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We propose an aerodynamic force decomposition which, for the first time, allows a thrust/drag bookkeeping in two-dimensional viscous and unsteady flows. Lamb-vector-based far-field methods are used at the scope, and the paper starts with extending recent steady compressible formulas to the unsteady regime.

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This page is a summary of: Aerodynamic force by Lamb vector integrals in unsteady compressible flows, International Journal of Numerical Methods for Heat &amp Fluid Flow, January 2024, Emerald,
DOI: 10.1108/hff-06-2023-0350.
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