Ethylene Flame Dynamics and Inlet Unstart in a Model Scramjet-Reference-Cited by-同舟云学术

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Ethylene Flame Dynamics and Inlet Unstart in a Model Scramjet

Published:2014-11 Issue:6 Volume:30 Page:1577-1585
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Liu Qili¹,Passaro Andrea²,Baccarella Damiano³,Do Hyungrok³

Affiliation:

1. Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, Indiana 46556-5684

2. Alta, S.p.A., 56121 Pisa, Italy

3. Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, Indiana 46556

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35214

Reference27 articles.

1. HeiserW. H.PrattD. T., Hypersonic Airbreathing Propulsion, AIAA Education Series, Washington, D.C., 1993, pp. 528–539.

2. Mach 6 Test of a Scramjet Engine with Boundary-Layer Bleeding

3. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

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