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
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R. Radespiel | K. Pausch | W. Schröder | V. Statnikov | M. Meinke | S. Stephan | M. Meinke | W. Schröder | R. Radespiel | V. Statnikov | K. Pausch | S. Stephan
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