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Verwundene Überschallflügel und Überschallflügel im Wirbelfeld

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Résumé

Calcul de l'écoulement supersonique linéarisé autour d'une aile rectangulaire vrillée à l'aide de la théorie des écoulements coniques. Application à un cas particulièrement simple de l'influence d'un filet toubillonnaire sur une aile rectangulaire.

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Literaturverzeichnis

  1. G. N. Ward,Linearized Theory of Steady High-Speed Flow (Cambridge University Press, 1955).

  2. P. Germain,La théorie générale des mouvements coniques et ses applications à l'aérodynamique supersonique (ONERA, Paris 1949).

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  3. A. F. Donovan undH. R. Lawrence,Aerodynamic Components of Aircraft at High Speeds (Princeton University Press, 1957).

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Authors and Affiliations

  1. Mitarbeiter am Service téchnique de l'Armée Française, Lörrach, Deutschland

    Carl Heinz

Authors
  1. Carl Heinz
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Heinz, C. Verwundene Überschallflügel und Überschallflügel im Wirbelfeld. Journal of Applied Mathematics and Physics (ZAMP) 9, 347–356 (1958). https://doi.org/10.1007/BF02424757

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  • DOI: https://doi.org/10.1007/BF02424757

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