Compressible unsteady aerodynamics for aeroelastic analysis of helicopter blades with trailing edge flaps and its implementation

Simple item page
dc.contributor.authorMyrtle, T.F.
dc.contributor.authorFriedmann, P.P.
dc.date.accessioned2016-08-15T13:51:29Z
dc.date.available2016-08-15T13:51:29Z
dc.date.issued1996
dc.identifier.otherERF-1996-Vol2-60
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3174
dc.language.isoen
dc.titleCompressible unsteady aerodynamics for aeroelastic analysis of helicopter blades with trailing edge flaps and its implementation

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
ERF-1996-Vol2-60.pdf
Size:
628.51 KB
Format:
Adobe Portable Document Format
Download

Collections

Papers