Summary
As part of the Joint International Vortex Flow Experiment, force and pressure measurements have been carried out on a 65 deg delta wing configuration in the transonic and supersonic wind tunnels of NLR. Out of these data three test cases were selected by the organizing committee of the GAMM WORKSHOP on the “Numerical Simulation of Compressible Euler Flows”. The paper discusses these test cases in more detail, as well as other features of this type of flow.
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References
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© 1989 Friedr Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig
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Elsenaar, A. (1989). The International Vortex Flow Experiment: A Test Case for Compressible Euler Codes. In: Dervieux, A., Leer, B.V., Periaux, J., Rizzi, A. (eds) Numerical Simulation of Compressible Euler Flows. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 26. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-87875-5_3
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DOI: https://doi.org/10.1007/978-3-322-87875-5_3
Publisher Name: Vieweg+Teubner Verlag
Print ISBN: 978-3-528-07626-9
Online ISBN: 978-3-322-87875-5
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