A Novel Supersonic Injection Scheme for Laser Induced Breakdown Ignition-Reference-Cited by-同舟云学术

A Novel Supersonic Injection Scheme for Laser Induced Breakdown Ignition

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 Aerodynamic Measurement Technology and Ground Testing Conference
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Author:

Lee Gyu Sub¹,Liu Qili¹,Baccarella Damiano¹,Elliott Gregory S.¹,Lee Tonghun¹

Affiliation:

1. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4286

Reference14 articles.

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4. The compressible turbulent shear layer: an experimental study

5. J. C. Dutton, "Compressible Turbulent Free Shear Layers," NATO Advisory Group for Aerospace Research and Development, no. Report No. AGARD-R-819, pp.2-1- 2-42,1997.

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