Characterization of ignition transient processes in kerosene-fueled model scramjet engine by dual-pulse laser-induced plasma
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference27 articles.
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2. 3D measurements of ignition processes at 20 kHz in a supersonic combustor;Ma;Appl. Phys. B,2015
3. Investigation of transient ignition processes in a model scramjet pilot cavity using simultaneous 100 kHz formaldehyde planar laser-induced fluorescence and CH* chemiluminescence imaging;Miller;Proc. Combust. Inst.,2017
4. Experimental investigation of ignition transient phase in model supersonic combustor;Xi;Proc. Inst. Mech. Eng.Part G: J. Aero. Eng.,2014
5. Investigation on ignition enhancement mechanism in a scramjet combustor with dual cavity;Li;J. Propul. Power,2016
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