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Inviscid, Incompressible Flow Past Thin Airfoils

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Abstract

The solution of the inviscid, incompressible and irrotational (potential) two-dimensional flow past an arbitrary profile with a sharp trailing edge exists and can be obtained using complex variables and mapping techniques. However, this approach is very difficult in general, except for particular classes of profiles, such as the Joukowski airfoils.

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References

  1. Glauert, H.: The Elements of Aerofoil and Airscrew Theory, 2nd edn. Cambridge University Press, Cambridge (1948)

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  2. Chattot, J.-J.: Optimization in applied aerodynamics. Comput. Fluid Dyn. J. 9(3), 306–311 (2000)

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  3. Drela, M.: MSES—Multi-element airfoil design/analysis software. http://raphael.mit.edu/research.html (1994)

  4. Chattot, J.-J.: Computational Aerodynamics and Fluid Dynamics: An Introduction. Scientific Computation. Springer, Berlin (2004)

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Correspondence to J. J. Chattot .

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Chattot, J.J., Hafez, M.M. (2015). Inviscid, Incompressible Flow Past Thin Airfoils. In: Theoretical and Applied Aerodynamics. Springer, Dordrecht. https://doi.org/10.1007/978-94-017-9825-9_3

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