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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)

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)

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)