Time-periodic shock interaction mechanisms over double wedges at Mach 7

A. S. Durna, B. Celik*

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

16 Citations (Scopus)

Abstract

The present study focuses on the long-term behavior of low-enthalpy M = 7 flows over double wedges that have a fixed fore angle of 30° and aft angles ranging from 45° to 60°. Although there are numerical and experimental studies available in the literature, they mostly consider the short-term behavior of such flows. In one of those studies, Durna et al. (Phys. Fluids 28:096101, 2016) foresee the presence of an aft angle threshold for transition from steady flow to complex shock–boundary layer interactions. The present study investigates the presence of periodicity by performing computations up to 50 times the duration of the previous study. Our analyses show that beyond a threshold value of 47°, the flows become time-periodic. We are able to describe complex interaction mechanisms of the periodic flow by utilizing the density gradients, shock locations, separation angle, and distributions of the pressure and heat flux over the wedge surfaces. The computational results show that as the aft angle is increased, the period of the flow shortens, and the duration, when the transmitted shock impinges on the wedge surface, decreases.

Original languageEnglish
Pages (from-to)381-399
Number of pages19
JournalShock Waves
Volume29
Issue number3
DOIs
Publication statusPublished - 7 Mar 2019

Bibliographical note

Publisher Copyright:
© 2018, Springer-Verlag GmbH Germany, part of Springer Nature.

Funding

Acknowledgements This study was funded by the projects of Istanbul Technical University (BAP, 39600) and TUBITAK (215M907). Computing resources used in this work were provided by the National Center of High Performance Computing of Turkey (UHEM) under Grant No. 5004292016.

FundersFunder number
TUBITAK215M907, 5004292016
British Association for Psychopharmacology39600
Istanbul Teknik Üniversitesi

    Keywords

    • Compressible flow
    • Shock–boundary layer interactions
    • Time-periodic motion

    Fingerprint

    Dive into the research topics of 'Time-periodic shock interaction mechanisms over double wedges at Mach 7'. Together they form a unique fingerprint.

    Cite this