Evolution of Large-Scale Structures Generated by a Strut Injector in a Mach 2.5 Flow-Reference-Cited by-同舟云学术

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Evolution of Large-Scale Structures Generated by a Strut Injector in a Mach 2.5 Flow

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Vergine Fabrizio¹,Maddalena Luca¹

Affiliation:

1. University of Texas, Arlington

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-332

Reference28 articles.

1. Enhanced mixing with streamwise vorticity

2. Growth of a Diffusion Flame in the Field of a Vortex

3. The round turbulent jet in a cross-wind

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1. Measurements of mixing layers and vortex structures of the strut-induced flow in a scramjet combustor with PIV and POD;Experimental Thermal and Fluid Science;2024-01

2. RANS Analysis of Merging Supersonic Streamwise Vortices for Enhanced Mixing in Scramjet Combustors;AIAA SCITECH 2022 Forum;2022-01-03

3. Hydrogen fueled scramjet combustor with a wavy-wall double strut fuel injector;Fuel;2021-11

4. Turbulent kinetic energy decay in supersonic streamwise interacting vortices;Journal of Fluid Mechanics;2016-10-19

5. The effect of vortex merging and non-merging on the transfer of modal turbulent kinetic energy content;Experiments in Fluids;2016-07-30

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