Abstract
We have seen that physically realistic transonic flow computations can be based on partial differential equations for the velocity potential and stream function that presuppose conservation of entropy. In terms of characteristic coordinates ξ and η we have
The coordinates ξ and n can be specified in terms of the speed q and the flow angle θ by the formulas
where f is any complex analytic function. Prescription of a second arbitrary function g serves to determine φ and ψ as solutions of the characteristic initial value problem
where ξ0 = η̄0 is a fixed subsonic point in the complex plane. With these conventions it turns out that <Inline>1</Inline> as can be seen from the uniqueness of the solution. Hence for subsonic flow the real hodograph plane corresponds to points in the complex domain where ξ0 = η̄0. To calculate φ and ψ paths of integration are laid down in the complex plane, and then a stable finite difference scheme is applied to solve the characteristic initial value problem (see Volume I).
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© 1977 Springer-Verlag Berlin Heidelberg
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Bauer, F., Garabedian, P., Korn, D. (1977). The Method of Complex Characteristics. In: Supercritical Wing Sections III. Lecture Notes in Economics and Mathematical Systems, vol 150. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-48852-8_2
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DOI: https://doi.org/10.1007/978-3-642-48852-8_2
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-08533-1
Online ISBN: 978-3-642-48852-8
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