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Numerical Simulation of Shock Boundary Layer Interaction Using Shock Fitting Technique

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Proceedings of XXIV AIMETA Conference 2019 (AIMETA 2019)

Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

Abstract

An unstructured, shock-fitting algorithm, originally developed to simulate Eulerian flows, has being further developed to make it capable of dealing with shock/boundary-layer interactions. This paper illustrates the algorithmic features of this technique and the results achieved in the computation of hypersonic flows past compression ramps.

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References

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Author information

Authors and Affiliations

  1. Dipartimento di Ingegneria Meccanica e Aerospaziale, Università degli Studi di Roma “La Sapienza”, Via Eudossiana, 18, 00184, Rome, Italy

    Alessia Assonitis & Renato Paciorri

  2. Scuola di Ingegneria, Università degli Studi della Basilicata, Viale dell’Ateneo Lucano 10, 85100, Potenza, Italy

    Aldo Bonfiglioli

Authors
  1. Alessia Assonitis
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  2. Renato Paciorri
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  3. Aldo Bonfiglioli
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Corresponding authors

Correspondence to Alessia Assonitis , Renato Paciorri or Aldo Bonfiglioli .

Editor information

Editors and Affiliations

  1. DIMA, Sapienza University of Rome, Rome, Italy

    Antonio Carcaterra

  2. DISG, Sapienza University of Rome, Rome, Italy

    Achille Paolone

  3. DIMA, Sapienza University of Rome, Rome, Italy

    Giorgio Graziani

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Assonitis, A., Paciorri, R., Bonfiglioli, A. (2020). Numerical Simulation of Shock Boundary Layer Interaction Using Shock Fitting Technique. In: Carcaterra, A., Paolone, A., Graziani, G. (eds) Proceedings of XXIV AIMETA Conference 2019. AIMETA 2019. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-41057-5_10

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  • DOI: https://doi.org/10.1007/978-3-030-41057-5_10

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-41056-8

  • Online ISBN: 978-3-030-41057-5

  • eBook Packages: EngineeringEngineering (R0)

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