Summary
A new design principle for transonic aerodynamics has led to several operational computer codes for shock-free flow. The method is described with emphasis on theoretical variable geometry definition of transonic airfoils and wings for efficient supercritical flight.
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References
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© 1980 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig
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Sobieczky, H. (1980). Computational Methods for the Design of Adaptive Airfoils and Wings. In: Hirschel, E.H. (eds) Proceedings of the Third GAMM — Conference on Numerical Methods in Fluid Mechanics. Notes on Numerical Fluid Mechanics, vol 2. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-86146-7_27
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DOI: https://doi.org/10.1007/978-3-322-86146-7_27
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-528-08076-1
Online ISBN: 978-3-322-86146-7
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