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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

Crossref DOI link: https://doi.org/10.1007/s12567-016-0112-x

Published Online: 2016-02-11

Published Print: 2016-06

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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