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Cited article:

Dynamics and spectral character of unsteady pressure field on afterbody of generic space launcher: Transonic flows

N.S. Vikramaditya and M. Viji
European Journal of Mechanics - B/Fluids 107 121 (2024)
https://doi.org/10.1016/j.euromechflu.2024.06.007

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

V. Statnikov, S. Stephan, K. Pausch, et al.
CEAS Space Journal 8 (2) 101 (2016)
https://doi.org/10.1007/s12567-016-0112-x