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Laminar boundary layer oblique shock wave interaction on flat and curved plates

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Résumé

Ce mémoire décrit quelques recherches expérimentales et théoriques sur l'interaction des ondes de choc obliques avec les couches limites laminaires. Une série de mesures détaillées de pressions et du frottement a été faite dans la région d'interaction dans un écoulement le long d'une plaque plane. Un modèle du mécanisme en a été déduit, dont les prédictions s'accordent raisonnablement bien avec les résultats des expériences. Les mêmes idées ont été appliquées à l'interaction sur une surface courbe, et les résultats s'accordent encore avec les expériences. Une étude simplifiée de la région de stabilité de l'interaction sous l'action d'oscillations de faible amplitude a été faite.

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References

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Authors and Affiliations

  1. Massachusetts Institute of Technology, Cambridge, Mass., USA

    Isaac Greber, Raimo J. Hakkinen & Leon Trilling

Authors
  1. Isaac Greber
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  2. Raimo J. Hakkinen
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  3. Leon Trilling
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Additional information

This work was supported by the National Advisory Committee for Aeronautics Contracts Nos. Naw-6320, 6412, 6452, 6507 and Air Force Contract No. 33-(616-3064) sponsored by the Wright Air Development Center, Wright Patterson Air Force Base.

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Greber, I., Hakkinen, R.J. & Trilling, L. Laminar boundary layer oblique shock wave interaction on flat and curved plates. Journal of Applied Mathematics and Physics (ZAMP) 9, 312–331 (1958). https://doi.org/10.1007/BF02424755

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  • DOI: https://doi.org/10.1007/BF02424755

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