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Flow Structures of Gaseous Jet in Supersonic Crossflow

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Jet in Supersonic Crossflow

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Abstract

Transverse injection into supersonic flow is one of the most fundamental canonical flows for supersonic propulsion community, which has been studied to enhance the understanding of supersonic turbulent mixing of jet fuel and combustion in scramjet engine combustors. It includes many flow features of interest, such as the three-dimensionality, the shock structures, the flow separation and recirculation, the wall-bounded free shear layer phenomenon, and the jet wakes.

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Authors and Affiliations

  1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan, China

    Mingbo Sun, Hongbo Wang & Feng Xiao

Authors
  1. Mingbo Sun
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  2. Hongbo Wang
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  3. Feng Xiao
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Correspondence to Mingbo Sun .

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Sun, M., Wang, H., Xiao, F. (2019). Flow Structures of Gaseous Jet in Supersonic Crossflow. In: Jet in Supersonic Crossflow. Springer, Singapore. https://doi.org/10.1007/978-981-13-6025-1_3

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  • DOI: https://doi.org/10.1007/978-981-13-6025-1_3

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-13-6024-4

  • Online ISBN: 978-981-13-6025-1

  • eBook Packages: EngineeringEngineering (R0)

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