Abstract
The unsteady aerodynamics is usually presented in terms of a relatively complicated integral equation where the unknown pressure jump appears within an integral over the wing system. This concept is introduced in this chapter.
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Notes
- 1.
The idea of separating the bound and free vortices can be found in the following publication: Walter Birnbaum, Das ebene Problem des schlagenden Flügels, Zeitschrift für Angewandte Mathematik und Mechanik, 1924.
- 2.
In this context the terminology “convection delay” is also used.
- 3.
H. L. Royden and P. M. Fitzpatrick, Real Analysis, Prentice Hall, 4th edition, ISBN-13: 978-8120342804, 2011.
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Demasi, L. (2024). Two-Dimensional Unsteady Incompressible Flow. In: Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity. Springer, Cham. https://doi.org/10.1007/978-3-031-50054-1_20
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DOI: https://doi.org/10.1007/978-3-031-50054-1_20
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