Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed

Simple item page
dc.contributor.authorBryce, W. W.
dc.date.accessioned2013-07-19T11:36:10Z
dc.date.available2013-07-19T11:36:10Z
dc.date.issued1956-11
dc.description.abstractA radial parabolic induced velocity distribution agreeing closely with flight measurements has been used for the hovering case. Continues...en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7988
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries110en_UK
dc.titleIndependence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speeden_UK
dc.typeReporten_UK

Files

Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
COA_Report_No_110_Nov_1956.pdf
Size:
4.49 MB
Format:
Adobe Portable Document Format
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.79 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

CoA. Reports