Abstract
Flow properties for supersonic flow around an inclined, flat plate were calculated employing the ‘Heartcurvemethod’. Calculations were performed for inclination angles that allowed supersonic flow to exist in the whole flow field. These limitations for the inclination angle were calculated. The most important results are given in diagrams.
The approximate solutions of M. J. Lighthill and K. Brieden were employed for the whole Mach number range and their solutions compared with the exact results. The deviations of these approximations from the exact results are shown in diagrams.
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Literaturverzeichnis
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Die Arbeit entstand am Institut für Aero- und Gasdynamik der Universität Stuttgart.
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Durst, F., Brieden, K. Die Überschallumströmung der angestellten, ebenen Platte. Journal of Applied Mathematics and Physics (ZAMP) 21, 947–962 (1970). https://doi.org/10.1007/BF01594853
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DOI: https://doi.org/10.1007/BF01594853