High Reynolds number helicopter fuselage test in the ONERA F1 pressurised wind tunnel

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dc.contributor.authorGatard, J.
dc.contributor.authorCostes, M.
dc.contributor.authorKroll, N.
dc.contributor.authorRenzoni, P.
dc.contributor.authorKokkalis, A.
dc.contributor.authorRocchetto, A.
dc.contributor.authorSerr, C.
dc.contributor.authorLarrey, E.
dc.contributor.authorFilippone, A.
dc.contributor.authorWehr, D.
dc.date.accessioned2016-08-15T13:51:53Z
dc.date.available2016-08-15T13:51:53Z
dc.date.issued1997
dc.identifier.otherERF-1997-35
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3244
dc.language.isoen
dc.titleHigh Reynolds number helicopter fuselage test in the ONERA F1 pressurised wind tunnel

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