Helicopter blade-vortex interaction noise reduction by active rotor control technology

dc.contributor.authorYu, Y.H.
dc.contributor.authorGmelin, B.
dc.contributor.authorSplettstoesser, W.
dc.contributor.authorPhilippe, J.J.
dc.contributor.authorPrieur, J.
dc.contributor.authorBrooks, T.E.
dc.date.accessioned2016-08-15T13:51:52Z
dc.date.available2016-08-15T13:51:52Z
dc.date.issued1997
dc.identifier.otherERF-1997-26
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3234
dc.language.isoen
dc.titleHelicopter blade-vortex interaction noise reduction by active rotor control technology

Files

Original bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
ERF-1997-26.pdf
Size:
789.25 KB
Format:
Adobe Portable Document Format

Collections