Hazards due to helicopter wakes

Kist, R. A.

dc.contributor.author	Kist, R. A.	en_UK
dc.date	1993	en_UK
dc.date.accessioned	2005-11-23T12:21:18Z
dc.date.available	2005-11-23T12:21:18Z
dc.date.issued	1993	en_UK
dc.identifier.uri	https://dspace.lib.cranfield.ac.uk/handle/1826/219
dc.description.abstract	The 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.sponsorship	The University	en_UK
dc.format.extent	1963 bytes
dc.format.extent	4565254 bytes
dc.format.mimetype	text/plain
dc.format.mimetype	application/pdf
dc.language.iso	en_UK	en_UK
dc.relation.ispartofseries	College of Aeronautics Report;9311	en_UK
dc.relation.ispartofseries	CU/CoA/R;9311	en_UK
dc.title	Hazards due to helicopter wakes	en_UK
dc.type	Technical Report	en_UK