Experimental and numerical results obtained at LABM and TSAGI on aerodynamic of helicopter rotor blades in hover

Simple item page
dc.contributor.authorBerton, E.
dc.contributor.authorFavier, D.
dc.contributor.authorMaresca, C.
dc.contributor.authorNsi Mba, M.
dc.contributor.authorVozhdaev, E.S.
dc.contributor.authorGolovkin, V.
dc.contributor.authorTarasov, N.N.
dc.contributor.authorMaslennikov, A.
dc.date.accessioned2016-06-29T16:19:44Z
dc.date.available2016-06-29T16:19:44Z
dc.date.issued2003
dc.identifier.otherp081
dc.identifier.urihttp://hdl.handle.net/20.500.11881/399
dc.language.isoen
dc.subject.otherAcoustics
dc.titleExperimental and numerical results obtained at LABM and TSAGI on aerodynamic of helicopter rotor blades in hover

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
p081.pdf
Size:
2.53 MB
Format:
Adobe Portable Document Format
Download

Collections

Papers