Reuse & Permissions

It is not necessary to obtain permission to reuse this article or its components as it is available under the terms of the Creative Commons Attribution 4.0 International license. This license permits unrestricted use, distribution, and reproduction in any medium, provided attribution to the author(s) and the published article's title, journal citation, and DOI are maintained. Please note that some figures may have been included with permission from other third parties. It is your responsibility to obtain the proper permission from the rights holder directly for these figures.

Export citation

Export citation

Choose format for download:

Download Citation
  • Gallery of Fluid Motion
  • Open Access
  • Access by Xinjiang University

Visualizations of direct fuel injection effects in a supersonic cavity flameholder

Hariswaran Sitaraman*, Nicholas Brunhart-Lupo, Marc Henry de Frahan, Shashank Yellapantula, Bruce Perry, Jon Rood, Ray Grout, Marc Day, Roba Binyahib et al.

Kenny Gruchalla

  • National Renewable Energy Laboratory, 15013 Denver West Parkway, Golden, Colorado 80401, USA

  • *Hariswaran.Sitaraman@nrel.gov

Phys. Rev. Fluids 6, 110504 – Published 15 November, 2021

DOI: https://doi.org/10.1103/PhysRevFluids.6.110504

Abstract

This paper is associated with a video winner of a 2020 American Physical Society's Division of Fluid Dynamics (DFD) Gallery of Fluid Motion Award for work presented at the DFD Gallery of Fluid Motion. The original video is available online at the Gallery of Fluid Motion, https://doi.org/10.1103/APS.DFD.2020.GFM.V0026.

View figure in article

Physics Subject Headings (PhySH)

Collections

This article appears in the following collection:

2020 Gallery of Fluid Motion

Collection of papers associated with the 2020 Gallery of Fluid Motion. These award winning works were presented at the annual meeting of the APS Division of Fluid Dynamics.

Article Text

References (7)

  1. D. B. Le, C. P. Goyne, R. H. Krauss, and J. C. McDaniel, Experimental study of a dual-mode scramjet isolator, J. Propul. Power 24, 1050 (2008).
  2. J. Taylor, F. Flanagan, A. Dunlop, S. D. Grimshaw, and R. Miller, Super aggressive S-ducts for air breathing rocket engines, J. Turbomach. 143, 061015 (2021).
  3. F. W. Barnes and C. Segal, Cavity-based flameholding for chemically-reacting supersonic flows, Prog. Aerosp. Sci. 76, 24 (2015).
  4. H. Sitaraman, S. Yellapantula, M. T. H. de Frahan, B. Perry, J. Rood, R. Grout, and M. Day, Adaptive mesh based combustion simulations of direct fuel injection effects in a supersonic cavity flame-holder, Combust. Flame 232, 111531 (2021).
  5. https://github.com/AMReX-Combustion/PeleC.
  6. Blender online community, Blender—A 3D modelling and rendering package (Blender Foundation, Blender Institute, Amsterdam, 2021).
  7. X. Zhang, A. Rona, and J. A. Edwards, The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer, Aeronaut. J. 102, 129 (1998).

Outline

Information

Sign In to Your Journals Account

Filter

Filter

Article Lookup

Enter a citation