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Effect of the Wave Structure of the Flow in a Supersonic Combustor on Ignition and Flame Stabilization
M. A. Goldfeld, Yu. V. Zakharova, A. V. Fedorov and N. N. Fedorova Combustion, Explosion, and Shock Waves 54(6) 629 (2018) https://doi.org/10.1134/S0010508218060011
Experimental and numerical investigations of the turbulent wake flow of a generic space launcher at $$M_\infty =3$$ M ∞ = 3 and $$M_\infty =6$$ M ∞ = 6