Hazards due to helicopter wakes

dc.contributor.authorKist, R. A.en_UK
dc.date1993en_UK
dc.date.accessioned2005-11-23T12:21:18Z
dc.date.available2005-11-23T12:21:18Z
dc.date.issued1993en_UK
dc.description.abstractThe local velocities induced in the wake of a helicopter can be a serious hazard to light aircraft operating nearby. A theoretical model is developed which makes it possible to estimate the rolling moment induced on a light aircraft entering the wake of a helicopter. The model shows good agreement with the limited amount of flight test data available. An annotated bibliography of the literature available on helicopter wakes is presented in order to identify specific areas in which further research is required.en_UK
dc.description.sponsorshipThe Universityen_UK
dc.format.extent1963 bytes
dc.format.extent4565254 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/219
dc.language.isoen_UKen_UK
dc.relation.ispartofseriesCollege of Aeronautics Report;9311en_UK
dc.relation.ispartofseriesCU/CoA/R;9311en_UK
dc.titleHazards due to helicopter wakesen_UK
dc.typeTechnical Reporten_UK

Files

Original bundle
Now showing 1 - 2 of 2
Loading...
Thumbnail Image
Name:
coareport9311.pdf
Size:
4.35 MB
Format:
Adobe Portable Document Format
No Thumbnail Available
Name:
license.txt
Size:
1.92 KB
Format:
Plain Text

Collections