Output details
15 - General Engineering
University of Glasgow
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Output 0 of 0 in the submission
Article title
Coupled thrust and vorticity dynamics during vortex ring state
Type
D - Journal article
Title of journal
Journal of the American Helicopter Society
Article number
022001
Volume number
54
Issue number
2
First page of article
1
ISSN of journal
0002-8711
Year of publication
2009
URL
-
Number of additional authors
2
Additional information
The research in this paper concerns the fluid dynamics associated with the critical flight regime encountered by helicopters in descending flight, known as the vortex ring state. There are very few examples of experimental work in this branch of fluid dynamics and so the paper is a data resource for rotorcraft designers and helicopter operators. This paper results from an international collaboration with the University of California, Berkeley, who part funded a Visiting Researcher post, and the US Army/NASA Rotary Wing Research Group (NASA Ames Research Center Grant NCC2-5507).
Interdisciplinary
-
Cross-referral requested
-
Research group
D - Aerospace Sciences
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
